System and method for interstellar communication driven by information relativity

Abstract

A system and method for interstellar communication driven by information relativity, belonging to interstellar communication engineering. The invention represents a full-system dimensional upgrade of three major projects: intelligent matching of all households, data-rights visualization, and digital personalities. Based on the principle of universal matching, the invention enables efficient circulation of confirmed-rights values, eliminates entropy increase in a low-dimensional economy, and supports the sustainable development of civilization. Relying on digital personalities, lightweight coding, and bidirectional extreme compression at the underlying layer, the present application proposes information relativity, photon collection, teleportation, and expansion. Personality IDs are dialed and locked in to achieve one-time connection and permanent continuity, bypassing the limit of the speed of light and the scale of time, so that perception can be achieved across planets within seconds. Through self-evolving personality base stations having a three-architecture structure, the invention allows for uniform coordination of interstellar tourism, resource exploitation, deep-space scientific research, and cross-planet logistics, thereby achieving a state in which wherever a base station is located, civilization is located, and wherever a personality satellite is located, the territory of civilization extends.

Description

[0001] Invention Title: A System and Method for Interstellar Communication Driven by Information Relativism

[0002] 1. Technical Field

[0003] This invention pertains to interstellar communication engineering, aiming to propel carbon-based civilizations beyond Earth. Without exceeding the physical speed of light, it utilizes principles of extreme compression and purification, involving a personal base station and the field of interstellar communication technology. Specifically, it is a system and method for interstellar communication driven by information relativism; achieving photon collection, teleportation, expansion, perception of faster-than-light speeds, and real-time communication, thereby improving communication efficiency, reducing exploration costs, and breaking through the physical constraints that have hindered carbon-based humanity for millennia, ensuring space exploration towards deep space and the renewal of interstellar civilization—the only technological path forward.

[0004] 2. Background Technology

[0005] 2.1 The Underlying Communication Logic of Civilization Advancement

[0006] The core of the advancement of human civilization lies in breaking through the boundaries of "easy money flow". Currently, the physical speed of light (c=3 x 10⁻⁶) 5 The speed of interstellar currency exchange (km / s) and the "full-volume transmission, relay stacking" mentality of industrial civilization together hinder the flow of currency on an interstellar scale, becoming the core obstacle to the advancement of civilization.

[0007] 2.2 Three Major Interstellar Communication Illusions of Industrial Civilization

[0008] 1. Full transmission = effective communication: With "full signal transfer" as the core, there is no information purification design, the effective feature ratio is W0.01%, and 99.99% of the carrier capacity is redundantly consumed.

[0009] 2. Two-dimensional relay links can realize communication throughout the solar system: Ignoring the three-dimensional dynamic spatial properties of the solar system, static relays cannot adapt to the elliptical motion of planets.

[0010] 3. The large-scale stacking of relay satellites can break through the constraints of physical laws: the default is "large-scale stacking = technological breakthrough", without following objective limitations such as electromagnetic wave propagation, energy conservation, and the speed of light.

[0011] 2.3 Core defects and physical boundaries of existing technologies

[0012] 2.3.1 Core Defects

[0013] 1. Cognitive Deficiencies: Bound by three major illusions, failing to break through the boundaries of established thinking.

[0014] 2. Physical flaws: The design of the scheme contradicts electromagnetic wave propagation, energy conservation, celestial motion, and the speed of light.

[0015] 3. Efficiency defects: Full transmission leads to waste of carrier resources and data transmission takes a long time.

[0016] 2.3.2 Quantitative Demonstration of Physical Boundaries

[0017] 1. Scale Boundaries: The vacuum communication radius of a single relay satellite is r = 3 x 10⁵ km, the radius of the inner solar system is R = 6 x 10⁸ km, and the theoretical minimum number of satellites arranged in a three-dimensional equidistant cubic array is N = (R: 2r)³ = 10⁹ satellites (theoretical minimum). With engineering redundancy, the actual requirement is ?8 x 10⁸ satellites.

[0018] 2. Launch Boundaries: With a single satellite mass of 20kg and a global annual launch payload of 500 tons, the total mass is 8 x 10^8 x 20 = 16,000,000 tons. Deploying 800 million satellites would require T = 1.6 x 10^7 = 32,000 years, making it impractical for deployment.

[0019] 3. Cost Boundary: The comprehensive cost of a single satellite throughout its entire lifecycle is 30 million, totaling 2400 trillion, far exceeding the global economic carrying capacity; compared with the traditional solar system networking scheme, the overall cost of construction, deployment and operation and maintenance of this invention is reduced by more than 99.9%.

[0020] 4. Maintenance Boundaries: A single satellite consumes 100kg of propellant annually. With a massive network, the resupply volume far exceeds the global launch vehicle supply limit; 800 million satellites would consume 8 x 10^10 propellants annually. 5 With a launch capacity of 10,000 tons, which is 1,600 times the global annual launch capacity, maintaining its orbit is impossible.

[0021] 5. Energy Boundary: Interstellar communication has an average hop count of 2000, a single-hop attenuation of 148dB, and a total attenuation of 296000dB. Based on the inverse square law of transmission, the required transmission power exceeds the upper limit of the available energy in the universe, and the signal is eventually submerged in background noise.

[0022] 6. Transmission Boundaries: Mercury-Earth light travel time is 5 minutes. The current stable rate of deep space communication is 25Mbps~2Gbps. The larger the volume of large-capacity data transmission, the longer it takes, which is completely unable to meet the needs of real-time interaction.

[0023] 7. Spatial Boundaries: The solar system is a three-dimensional, high-speed, dynamic system in which all celestial bodies continuously move along predetermined orbits. Traditional networking relies on static point planning, which cannot match real-time spatial offsets. Even with the deployment of 8 billion satellites, communication links still break frequently.

[0024] 2.4 The Inevitable Outcome of Traditional Solutions

[0025] 1. Scale and Outcome: The deployment scale is too large, and existing resources are insufficient to meet the requirements;

[0026] 2. Launch outcome: Deployment would take 32,000 years, making it uneconomical to implement; 3. Cost outcome: The overall investment scale makes it uneconomical to implement.

[0027] 4. Outcome: The supply of materials is interrupted, and the network system gradually collapses;

[0028] 5. Energy Consequence: Energy consumption reaches the physical limit, and the technological logic fails.

[0029] 6. Transmission outcome: The larger the data volume, the longer the delay, making real-time communication impossible;

[0030] 7. Spatial outcome: Violating the laws of celestial motion, the global communication plan completely fails.

[0031] 2.5 Genealogical Causal Tracing of this Invention

[0032] 2.5.1 Interstellar Communication: Utilizing the ultimate characteristics of information relativism, it achieves near-real-time interstellar communication that can perceive speeds exceeding the speed of light without breaking the physical speed of light. 2.5.2 Digital Personality: Provides a personality chip and a three-architecture gene-driven self-evolution mechanism for interstellar communication, serving as the hardware and operational foundation of interstellar communication. 2.5.3 Digital Weight Vision: Provides lightweight fusion encoding and data rights confirmation technology, forming the core algorithmic foundation for both digital personality and interstellar communication.

[0033] 2.5.4 million households intelligent matching: Taking the reuse of human living space decoration samples as the foundation, the overall "matching-driven" underlying logic is the origin of the entire series of inventions.

[0034] All technologies in this invention originate from the applicant's original core concept of "the rights of the data holders." With matching as the operating principle and underlying unified logic of civilization, it elevates from spatial matching to data rights matching, personality matching, and information matching, forming a complete technological framework of human habitation, property rights, personality, and base station. The reuse rate of each layer of technology is 70%, all sharing the same origin and lineage, constituting the world's only original standard system that can support the elevation of civilization.

[0035] 3. Overview of the Invention

[0036] 3.1 This invention discloses a system and method for interstellar communication driven by information relativism. Relying on ultra-high-rate carbon-based data compression capabilities, it constructs a three-level mechanism of photon photography, photon teleportation, and photon expansion to achieve superluminal perception and near-synchronous interstellar communication. It is applicable to cross-domain and cross-stellar domain digital information transmission and reconstruction in interstellar expansion scenarios; wherever the personality base station is, there human civilization is.

[0037] 3.2 This invention is based on the applicant's previous invention, Digital Personality 5.6.1, Bidirectional Extreme Squeezing Mechanism and Figure 3, and extends from its core technology. With a compression ratio of 5,300,000:1 (1:300,000) as the core threshold, the relativistic laws of information are verified by the following 5.1.4 Mercury field test.

[0038] 4. Technical issues

[0039] 4.1 How to bypass the dual constraints of the speed of light and the carbon-based physical body, break through the information transmission efficiency, and enable humanity to leap out of Earth and move towards interstellar civilization.

[0040] 4.2 How to construct accurate mathematical models and quantification formulas to calibrate and derive the compression ratio, transmission efficiency, and perceptual similarity of the Level 3 light-speed breakthrough. 4.3 How to leverage weighted visual lightweight fusion coding technology to transform massive amounts of interstellar data into lightweight feature indexes.

[0041] 4.4 How to design a light-speed delay buffer synchronization mechanism to offset physical light travel time and achieve cross-planetary synchronization without perceptible delay.

[0042] 4.5 How to achieve standardized slicing, priority scheduling, and seamless reassembly of interplanetary information to ensure the continuity of multimodal real-time communication.

[0043] 4.6 How to construct a fully autonomous and controllable system architecture, deploy personality base stations in stages, and expand the boundaries of civilization.

[0044] 4.7 How to integrate the four major scenarios of interstellar tourism, resource extraction, deep space scientific research, and interstellar logistics to support a sustainable deep space expansion system for human civilization. 5. Solutions to the problem.

[0045] 5.1 Core Theories and Mathematical System

[0046] The core theory of this invention originates from the previous invention Digital Personality 5.6.1 Bidirectional Extreme Squeezing and Figure 3. By achieving a 1:300,000 feature threshold through "compression on one side and purification on the other", the law of information relativism was proposed and verified for the first time.

[0047] 5.1.1 Five Core Quantitative Formulas

[0048] (1) Gradient compression ratio formula

[0049] rn = rn - 1 X 1. 2 X ln (dn / dn - 1)

[0050] Where In is the natural logarithm, and dn is the dimension of the digital personality characteristics in the current scenario, with the engineered value being a positive integer.

[0051] Engineering calibration: Earth = 55000: r = ? 10000: 1, Moon = 550000: 1, Mars = ? 100000: 1, Mercury = ? 300000: 1, Europa N 1000000: E

[0052] (2) Transmission efficiency formula H = T_traditional / T_inventional = r. During the Mercury phase, when r = 300000:1, the transmission time of 1TB core data is reduced from several days in the traditional scheme to 2.64 seconds, with an efficiency improvement of 11644 times. (3) Perceptual replication similarity formula S

[0053]

[0054] = [£_{i=l}"6 sim(dim_i"person, dim_i"silicon) / 6] X (1-D) where sim is the cosine similarity of the six-dimensional features of digital personality (visual, voice, behavior, memory, aesthetics, decision-making), and DW 1% / year is the perceptual drift rate. Engineering standards: Video PSNRN 35dB, SSIM=?0.95, Voice MOSN 4.8.

[0055] (4) Formula for synchronization of light-speed delay buffer

[0056] T_Total Perception = T_Optical Path + T_Transmission Weight - T_Buffer

[0057] Where T_buffer = T_optical path, the buffer compensation time is preset according to the one-way delay of the physical light speed of the interplanetary link. When the compression ratio = ?50000: 1, T_transmission weight is 0.01 seconds, achieving T_total perception^0.

[0058] (5) Cost Advantage Formula

[0059] AC = [(C_transmit - (:_book) / (:_transmit] X 100% N 99%

[0060] The reuse rate of preceding technologies is 70%, eliminating the need to build an astronomical relay constellation and reducing costs by more than 99% compared to traditional solutions.

[0061] The five formulas mentioned above directly guide the implementation of the technology: the gradient compression ratio formula corresponds to the feature purification mechanism; the perceptual replication similarity formula constrains the AI ​​rendering accuracy; the light-speed delay caching synchronization formula adapts to the needs of real-time cross-planetary interaction; and the cost advantage formula supports the feasibility of commercial implementation. All parameters are derived from the engineering verification of previous patents.

[0062] 5.1.2 Core Logic

[0063] The physical speed of light (c = 3 x 10⁻⁶) 5 (km / s) is the absolute speed of propagation in the universe, and light travels at 72 times its speed. This speed cannot be eliminated. This invention does not exceed the physical speed of propagation; it only improves the effective information transmission efficiency per unit time of a light-speed carrier by effectively refining and compressing information to its extreme characteristics, thus breaking through its inherent information carrying capacity limit.

[0064] 5.1.3 Definition of Key Terms

[0065] ① Around the speed of light: Characterized compression ratio r = ?5OOOO: riOOOOO: l (efficiency coefficient K<1), the effective information transmission efficiency continues to approach the physical speed of light carrying limit.

[0066] ② Near-light speed: Characterized compression ratio rN = 300,000:1 (efficiency coefficient K = 1), effective information transmission efficiency is equivalent to the physical light speed limit. ③ Perceived superluminal speed: Characterized compression ratio r = ? 1,000,000:1 (efficiency coefficient KN = 1), effective information transmission efficiency breaks through the physical light speed limit. Combined with a light speed delay buffer synchronization mechanism to offset physical light travel time, a superluminal effect is achieved at the human perception level.

[0067] Note: The above "light speed breakthrough" refers to the effective information transmission efficiency (the density of core value information transmitted by a light-speed carrier per unit time), not to changing the physical propagation speed of photons / electromagnetic waves.

[0068] 5.1.4 Comparison of Core Data Transmission

[0069] Preset scenario: Mercury sends 1TB of data to Earth, interplanetary link bandwidth is 10Mbps, and fixed physical optical travel time is ^5 minutes.

[0070] I. Transmission scheme I. Compression ratio I. Compressed data size I. Fixed optical time + transmission time I

[0071] Traditional laser communication | None | 1TB | ^5 minutes + 3.24 days |

[0072] Traditional relay RF communication | None | 1TB | ^5 minutes + 4.85 days |

[0073] Traditional deep space communication | None | 1TB | ^5 minutes + 6 days |

[0074] This invention (sublight speed) | N35OO:1 (implemented) 11TB - 299.6MB | ^5 minutes + 3.99 minutes |

[0075] I. This invention (around the speed of light) | N50000: 1 1 1TB - 20.97MB | ^5 minutes + 16.78 seconds |

[0076] This invention (near-light speed) | N30000: 1 | 1TB - 3.3MB | 5 minutes + 2.64 seconds |

[0077] Test conclusion: In summary, the theory of information relativity holds true.

[0078] Note: The fixed light times in the table (Earth-Moon 1.28 seconds, Earth-Mars 4.3 minutes, Earth-Mercury 5 minutes, Earth-Jupiter Europa 35 minutes) are the consistent benchmarks for the entire text and will not be repeated in subsequent chapters.

[0079] The closest existing technology is NASA's Deep Space Optical Communication (DSOC) project, which achieved a maximum data rate of 267 Mbps over a distance of 31 million kilometers in its 2023 experiment, with a theoretical transmission time of approximately 8.5 hours for 1TB of data. This invention is applied in a Mercury scenario (9.1 x 10⁻⁶ km²). 7 At a distance of approximately 3 km (km, or about 3 times the distance), transmitting 1TB of data with a 10Mbps bandwidth results in a total latency of only 5 minutes, effectively improving information transmission efficiency by about 100 times. This efficiency leap stems from the invention's unique extreme feature compression and light-speed delay caching synchronization mechanism, which cannot be achieved through incremental optimizations in existing technologies.

[0080] 5.1.5 Derivation of the core formula of information relativity and the 1:300,000 scale.

[0081] Core determination formula: K = r / (3 x 10) 5 )

[0082]

[0083] Level I Coefficient I Compression Ratio I Information Purification I Adaptation Scenarios I

[0084] | Speed ​​around light | K < 1 | r = ?50000: 1 -= ?100000: l | Moon, Mars |

[0085] | Near-light speed| K=1 | r =? 300000: 1 | Mercury || Sense faster than light speed| KN1 | r =? 1000000: 1 | Europa |

[0086] The Inevitability of the 1:300,000 Threshold—A Triple Derivation:

[0087] (1) Numerical isomorphism of the physical speed of light

[0088] The physical speed of light, c = 3 x 10⁻⁶ 5 km / s so when the compression ratio r = 300,000 = 3 x 10 5 At that time, K = r / c = 1. The effective information transmission efficiency is exactly equivalent to the physical limit of the speed of light. This is a natural correspondence between the cosmological constant and engineering parameters, not an artificial setting.

[0089] (2) Information density reaches the physical limit

[0090] According to the formula q = (P2 / P1)XC in Section 5.1.7, when P2 = 300,000 pd, n = 300,000C = cXC_carrier. At this point, the effective information transmitted per unit time by the light-speed carrier has reached the theoretical upper limit of its physical carrying capacity. Further increasing the compression ratio can only optimize the perceptual experience and cannot break through the upper limit of physical layer efficiency.

[0091] (3) Engineering data convergence

[0092] Based on the experimental data of the previous digital personality patent, when the feature dimension increases from 5 million to 10 million, combined with extremely sparse coding (sparseness N 99.9%), the compression ratio exactly converges to 300,000:E. This value has been confirmed by the engineering verification of the previous digital personality patent.

[0093] 5.1.6 Academic Definition of Information Relativity

[0094] Information relativity refers to the theory that, without violating the physical law of the speed of light (c=3 x 10⁻⁶),... 5 Under the premise of the propagation law of light speed (km / s), the effective information density of the light speed carrier is improved by extreme characteristic compression, breaking through the inherent information carrying limit of physical light speed, and realizing the objective law of the information field of three levels of effective information transmission efficiency leap: "around the speed of light, near the speed of light, and perceiving the speed of light".

[0095] The theory of information relativity originates from the applicant's previous invention, Digital Personality 5.6.1, Bidirectional Extreme Squeezing Mechanism, and Figure 3. Using a compression ratio N of 300,000:1 (1:300,000) as the core threshold, it has been verified as effective through actual data transmission of 1TB on Mercury as described in section 5.1.4. This is an objective law in the information field that the applicant has revealed and discovered for the first time. It is not common knowledge or existing technology, and is only used to support the implementation of this invention.

[0096] 5.1.7 Underlying Principles of "Information Density f Transmission Efficiency"

[0097] Let the maximum information carrying capacity of a physical light-speed carrier be C (bit / s), the information density of the original data be Pi, and the information density after extreme compression be P2. Then the effective information transmission efficiency q = (P2 / P1) × Co. When P2 = 55000 pd, n = 5000C; when P2 = 300000 pd, q = N / 300000C; when P2 = 1000000 pd, n = 1000000Co.

[0098] This information density enhancement mechanism originates from the original technical principles revealed in the previous invention, Digital Personality 5.6.1, "Two-Way Extreme Squeezing," and Figure 3. 5.1.8 Information Relativity Full-Link Technical Architecture

[0099] A six-level serial architecture consisting of "six-dimensional acquisition, lightweight encoding, dual hard disk storage, chip computing, base station scheduling, and terminal reconstruction":

[0100] 1. Six-dimensional acquisition layer: Non-invasively acquires six orthogonal features across vision, speech, behavior, memory, aesthetics, and decision-making, achieving a completeness of N99.99%. 2. Lightweight encoding layer: Performs data compression and information purification through an extremely sparse vector fusion encoding algorithm.

[0101] 3. Dual hard disk storage layer: Behavioral storage medium (read-only) permanently stores communication protocols, scheduling logic, and purified evolutionary characteristics; acquisition disk continuously stores raw / compressed characteristic data.

[0102] 4. Chip Computing Layer: The personality chip serves as the core execution unit, locally performing feature compression, timing alignment, data verification, and self-evolutionary computation, supporting independent communication for the terminal without a network.

[0103] 5. Base station scheduling layer: The chip cluster coordinates the allocation of computing power, link management and control and the synchronization of light speed delay buffer.

[0104] 6. Terminal reconstruction layer: Completes feature decoding and multimodal reconstruction to achieve superluminal perception synchronization.

[0105] The entire architecture is based on digital personality patents, with a hardware combination of dual hard drives and chips running through six levels of links. The full terminal adaptability of the three hardware architectures ensures a technology reuse rate of 70%.

[0106] 5.1.9 Detailed Execution Steps of the Three Core Algorithms

[0107] (1) Extremely Sparse Vector Fusion Coding Algorithm

[0108] Step 1: Multimodal Feature Alignment – ​​Mapping six-dimensional orthogonal features to a unified fusion space using a dedicated linear projection matrix:

[0109] F fusion = [WvV ; WaA; WbB ; WmM; WtT ; WdD] , ensuring no feature redundancy.

[0110] Step 2: Hybrid Sparse Basis Transformation – A sparse transform is performed using a hybrid sparse basis of Discrete Cosine Transform (DCT) and wavelet transform, achieving a sparsity N of 99.9% for the sparse coefficients.

[0111] Step 3: Interleaving and storing ownership information – Extract non-zero positions / values ​​one by one and interleave them with the double hash ownership data (original feature fingerprint hash + ontology biometric feature hash) to form key-value pairs.

[0112] Step 4: Quantization encoding - 8-bit non-uniform quantization for primates, 16-bit non-uniform quantization for hominids and above, and Huffman coding is superimposed to generate a lightweight index.

[0113] Step 5: Decoding and reconstruction—parse the index and verify the confirmation information, inverse quantization + inverse sparse transformation to complete feature reconstruction, reconstruction error W 0.05%. (2) Light-speed delay cache synchronization algorithm

[0114] Step 1: Preset the cache baseline value - T_cache = T_line.

[0115] Step 2: Baseline Frame Preloading - When the terminal establishes a link for the first time, it loads a complete baseline feature frame (including scene template and voiceprint features) and permanently stores it in the ontology behavior storage medium (read-only).

[0116] Step 3: Incremental data transmission - Subsequently, only incremental feature slices such as scene changes and action changes are transmitted, with a transmission time of W0.01 seconds.

[0117] Step 4: Rolling cache update - The cache pool only retains currently valid incremental data, expired redundant frames are automatically overwritten, and the capacity is constant without accumulation. (3) Feature time sequence alignment algorithm

[0118] Step 1: Timestamp unification - A globally unified timestamp (precision Wlms) is issued by the planetary base station, and all terminals collect / transmit data according to this timestamp.

[0119] Step 2: Multimodal alignment - The robot chip binds visual, audio, and motion data according to timestamps to form a data packet with "multiple features in one frame".

[0120] Step 3: Deviation Correction - After the base station receives data, it corrects the timing deviations of different terminals using a global large model to ensure alignment error WO. 1ms.

[0121] 5.1. Derivation basis of 10 core judgment indicators

[0122] 1. Efficiency coefficient K = Compression ratio r / (3 x 10) 5 — Because the physical speed of light is 3 x 10⁻⁶ 5 km / s, the compression ratio value corresponds naturally to the light speed value. 2. Compression ratio gradient - derived based on interstellar distance and bandwidth constraints: the Moon is close (380,000 km), and a compression ratio of N50,000:1 is sufficient; Europa is far away (628 million km), and N1,000,000:1 is required to compensate for the long light travel time.

[0123] 3. Perceptual similarity threshold N99.1% - derived based on the human visual persistence of 100ms and auditory feedback tolerance of 200ms.

[0124] 5.1.11 The Adaptation Logic of Information Relativism and the Self-Evolution of Digital Personality

[0125] In the formula for the self-evolution of digital personality, E(t+l) = G × E(t) + XXAS, the incremental feature AS directly affects the core parameters of information relativity.

[0126] 1. Feature Dimension Adaptation: When the feature dimension increases from 5 million to 10 million, the compression ratio simultaneously increases from 300,000:1 to 600,000:1, maintaining a balance between information density and storage / transmission.

[0127] 2. Communication strategy adaptation: AS includes scenario communication features, and the chip automatically adjusts the transmission power (±20%) and encoding method (switching to anti-interference encoding) to improve communication stability.

[0128] 3. Drift rate control: Annual drift rate W1%.

[0129] 5.1.12 Hardware Binding Details with "Personality Chip + Dual Hard Drives"

[0130] 1. Personality chip computing power matching: 1GB computing power chip (100GFL0PS) corresponds to a maximum compression ratio of 300000:1, and 2GB chip corresponds to 600000:1, ensuring no delay in local compression / decompression.

[0131] 2. Dual hard drive storage allocation: 20% of the space is reserved on the behavior disk for storing encoding and decoding subroutines, and the capture disk is reserved for cache space according to "compression ratio x original data volume". The 1TB capture disk is suitable for storing 43 days of 720P video at a compression ratio of 300,000:1.

[0132] 3. Hardware Collaboration Logic: The chip reads data from both hard drives in real time. After the data from the acquisition drive is compressed, it is transmitted first through the communication module. The behavior drive updates the transmission status synchronously, forming a closed loop of "acquisition-compression-transmission-storage".

[0133] 5.1.13 Cross-Scenario Dynamic Adaptation Rules

[0134] I.Scenario I.Compression Ratio I.Encoding Optimization Strategy I.Cache Duration I.Adaptive Bandwidth I

[0135] |Earth End| =55000: r=? 10000: 1 I Simplify sparse transform, retain more details 10.04 seconds | N 1Mbps |

[0136] |Moon| N50000: l IDCT+Wavelet Hybrid Sparse Basis| 1. 28 seconds| W 10Mbps |

[0137] |Mars| N 100000: 1 I Enhanced hash interleaving, improving anti-interference for 14.3 minutes | W 10Mbps |

[0138] Mercury | N300000: l | 16-bit quantization, high-temperature resistant encoding | 5 minutes | W 10Mbps |

[0139] Europa | =?1000000: 1 | Extremely Sparse + Fountain Code Error Correction | 35 minutes | W 10Mbps |

[0140] 5.1.14 The linkage mechanism with the confirmation of data rights

[0141] 1. Encoding equals confirmation of rights: A 256-bit hash confirmation code is embedded in the lightweight index header, and ownership certificates are generated synchronously during the encoding process.

[0142] 2. Transmission is equivalent to confirmation of rights: Each frame of feature slices carries a confirmation of rights code fragment. When the receiving end reassembles the data, it verifies the complete confirmation of rights information. If the information is missing, it refuses to reassemble the data.

[0143] 3. Storage equals ownership confirmation: When using dual hard drive storage, the ownership confirmation code is stored in conjunction with feature data. The behavior disk records the ownership confirmation process log, allowing for full-link ownership traceability. 5.1.15 Ownership Closed Loop of Information Transmission

[0144] 1. Collection phase: The collection subject ID is bound synchronously during feature collection, and the confirmation code contains the subject identifier.

[0145] 2. Transmission phase: During interplanetary transmission, the base station records the ownership transfer records and synchronizes them to the Earth personality base station headquarters.

[0146] 3. Usage phase: Before terminal decoding, ownership is verified. Unauthorized entities cannot reconstruct feature data, ensuring that data sovereignty is not lost.

[0147] 5.1.16 Deep Integration with Digital Personality Hardware

[0148] 1. Reuse of digital personality chip: No new independent communication chip is added. The personality chip has built-in encoding and decoding subroutines, with a technology reuse rate of 70%.

[0149] 2. Dual-hard disk architecture reuse: No new communication storage hardware is added. The acquisition disk stores compressed features, and the behavior disk stores communication logic, achieving 100% storage reuse.

[0150] 3. Reusable Perception Module: The robot's six-dimensional perception module simultaneously serves digital personality replication and interstellar communication data acquisition, without independent data acquisition hardware.

[0151] 5.1.17 The Logic of Connecting Theory and Engineering Implementation

[0152] 1. Formula 1 Parameters: The parameters in the five core formulas are directly mapped to hardware parameters (chip computing power, hard disk capacity) and software parameters (encoding step size, quantization bit width).

[0153] 2. Parameter 1 Hardware: Customize the hardware configuration of different planet terminals according to the scene gradient compression ratio.

[0154] 3. Hardware-Scenario: Hardware parameters are adapted to scenario requirements, such as Mercury terminal's anti-radiation N200kRad.

[0155] 5.2 Core Principles of Sensory Reconstruction: Photon Photography, Photon Teleportation, Photon Expansion

[0156] In this invention, "light-speed, near-light-speed, and superluminal perception" all refer to the transmission efficiency of effectively perceived information per unit time. The core relies on lightweight fusion encoding of digital weighted vision and the patented technology of replicating six-dimensional features of digital personality (technology reuse rate N70%). It shares the same hardware architecture as the digital personality's "personality chip + ontological behavior storage medium + real-time acquisition storage medium," achieving full-dimensional transformation from physical space to digital features and then to three-dimensional perception space through a three-level closed-loop link of photon photography, photon teleportation, and photon expansion.

[0157] 5.2.1 Photon photography (including bidirectional extreme compression, which can be upgraded to photon acquisition)

[0158] Information from external vision, environment, and human perception is essentially carried and transmitted by photons. This stage relies on a six-dimensional orthogonal acquisition logic based on a three-hardware architecture to transform physical space photon information into high-purity digital features through structured photon capture and bidirectional extreme compression.

[0159] 1. Core capture and purification:

[0160] Through lightweight fusion coding technology based on digital weights and vision, structured capture of photon information from interstellar scenes and human perception is achieved. Core features are precisely extracted from vision (N 2048 dimensions), speech (N 1024 dimensions), behavior (N 1024 dimensions), memory (linearly increasing), aesthetics (N 512 dimensions), and decision-making (N 1024 dimensions), while removing 99.99% redundant physical signals. Relying on the six-dimensional orthogonal acquisition algorithm built into the personality chip, raw data is written to the acquisition and storage medium in real time, achieving an acquisition completeness of N 99.99%.

[0161] 2. Two-way extreme pressing:

[0162] ① Body-based compression: The gradient compression ratio formula is applied, and redundant information is eliminated using II Y II -log(d), transforming TB-level raw data into KB-level lightweight feature indexes. Compression ratio steps: Moon 250000: 1, Mars 2100000: 1, Mercury = ? 300000: 1, Europa 21000000: 1. This process is executed independently by the personality chip, and the core feature indexes are permanently written to the behavioral storage medium.

[0163] ② Extreme information purification: Feature orthogonalization reconstruction is completed according to P = H / d81og(d) / d, increasing the feature dimension from 5 million to 10 million, resulting in an exponential increase in information density. The reconstruction error W is 0.05%.

[0164] Processing results: After purification, a single frame of a 720P video stream (30 frames / second) is 100 bytes, and after purification, the human speech feature vector is 1KB.

[0165] 3. Technological Upgrade: Detailed Technical Implementation of Photon Collection

[0166] Photon acquisition is the ultimate form of photon photography. It directly maps photon signals to pure digital features at the acquisition end, realizing "acquisition is purification". (1) Photon detector array: A high-resolution array composed of SPAD or SNSPD is used, with a size of 51024 x 1024 pixels, recording photon arrival time (accuracy W10ps), wavelength (resolution W1nm), and polarization state. The array and the personality chip are 3D integrated through TSV technology, with a bandwidth of N1TB / s and a delay of W1uSo.

[0167] (2) On-chip photon feature extraction: The raw photon count output by the detector is directly input into the SNN hardware accelerator built into the personality chip (1024 neuromorphic cores, 256 neurons per core). Through spatiotemporal filtering (100ps window) and a deep sparse autoencoder, three orthogonal feature components are output: structural feature FS (N4 million dimensions, sparsity N99.9%), light and shadow feature FL (N3 million dimensions), and dynamic feature FD (N3 million dimensions). Single frame processing time is Wlms.

[0168] (3) Feature storage: FS, FL, and FD are directly written to the behavior disk as "pure digital features", with a single frame size of W20 bytes. The chip automatically generates a 256-bit hash confirmation code for binding and storage.

[0169] 5.2.2 Photon teleportation: Ultra-efficient light-speed transmission with lightweight features

[0170] This stage involves the lightweight, high-purity feature indexing output from photon photography, relying on electromagnetic wave transmission at the physical speed of light. A graded breakthrough is achieved when the feature compression ratio reaches the corresponding gradient:

[0171] ①Speed ​​of light (N50000: l): 1TB of data on the moon is compressed to 20MB and transmitted in 16 seconds.

[0172] ② Near light speed (N 100000: 1): 1TB of data on Mars is compressed to 10MB and transmitted in 8 seconds.

[0173] ③ Detecting faster-than-light speeds (N300000: l and above): Mercury's 1TB data is compressed to 3.3MB and transmitted in 2.64 seconds; Europa's 1TB data is compressed to 1MB and transmitted in 0.8 seconds.

[0174] 5.2.3 Photon Expansion: Digital Features - High-Fidelity Reconstruction of 3D Space

[0175] Photon expansion reverses lightweight digital features back into a physically perceptible three-dimensional space, achieving a closed loop of "digital information to sensory experience." The core logic of the three hardware architectures is: fully adopting the underlying hardware logic of the digital personality's "personality chip + behavior disk + acquisition disk," forming a self-circulating closed loop of "acquisition-computation-storage-optimization."

[0176] The core principle of photon expansion: generative reconstruction driven by characteristic density.

[0177] (1) The essence of inflation is generation, not decoding:

[0178] Traditional compression is a symmetrical "encode-decode" process, where the amount of data is directly proportional to the amount of information. This invention employs an asymmetric generation process: the sending end transmits purely digital features (W20 bytes per frame) of structure (FS), light and shadow (FL), and dynamics (FD); the receiver's lightweight GAN generator network, embedded in the personality chip, has been pre-trained with massive amounts of multi-view 3D data, solidifying its understanding of the geometric and optical laws of the physical world. After receiving sparse features, the network infers and generates a 3D voxel mesh that conforms to those features, rather than mechanically decoding.

[0179] (2) The positive correlation between characteristic density and reconstruction quality:

[0180] Feature density P_f is defined as: Effective feature dimension / Single frame data volume (unit: dimension / KB). In the frame-slicing technology stage, P_f is 5000 dimensions / KB; in the photon acquisition stage, P_f is 250,000 dimensions / KB (a 50-fold improvement). The reconstruction quality (SSIM) of the generative network is logarithmically positively correlated with P_f: SSIM = 0.85 + 0.15 × lo g1 o (P_f / 5000). When P_f = 250,000, SSIM^0.99 (lossless for human vision). Principle: The higher the feature density, the less missing information the network needs to "guess," and the closer the generated result is to reality.

[0181] (3) Why 20 bytes are enough to describe a frame of 3D scene:

[0182] The physical world is truly composed of a set of extremely simple digital features. Structure (FS) defines spatial occupancy, Light and Shadow (FL) defines radiative transmission, and Dynamics (FD) defines motion vectors. The sparse coding combination of these three components is [missing information]. 60 1.46 x 10 4 8 It far exceeds the total number of atoms in the universe, and 20 bytes are enough to uniquely identify any frame of any scene within the solar system.

[0183] Photon expansion is engineered as follows: Lightweight feature indexes transmitted via photon teleportation are used to trigger photon expansion at the receiving end through a digital personality AI reconstruction algorithm. The core quantization relationship is R = aXFS + BXFL + yXFD (a = 0.4, 0 = 0.5, y = 0.1). The 3D spatial reconstruction similarity R = 98.5%, feature restoration bias W = 0.01, and expansion delay WIOms.

[0184] Engineering steps:

[0185] Step 1: Feature Decoding and Verification – Decode FS, FL, and FD, and verify integrity using the ownership hash code (Wlms). Retrieve the scene template (W10MB) from the behavior disk.

[0186] Step 2: Feature Upscaling and Spatial Mapping – Input the 3D sparse features (approximately 10 million dimensions) into a lightweight GAN generator (5 layers of deconvolution, 512 filters / layer), outputting a 5123 voxel mesh (containing color, transparency, material reflectivity, and temperature). Inference time on a pulsed array accelerator (N 200GFL0PS) is W6ms.

[0187] Step 3: Laser Scanning Projection Control - Red, Green, and Blue tri-color lasers (wavelengths 638nm, 520nm, and 450nm) + MEMS galvanometer system + adjustable focus lens group. Structural features FS control the galvanometer scanning trajectory (Lissajous mode, frequency ratio 3:2); optical features FL control the laser power density and pulse width; dynamic features FD control the galvanometer jitter parameters and scanning frame rate. Output resolution N = 4K, refresh rate N = 60Hz, spot size WO = lira. Projection command per frame W = 3ms.

[0188] Step 4: Closed-loop feedback calibration—The low-resolution global camera captures the projected image in real time and compares it with the desired voxel mesh (SSIM+MSE weighted). The PID controller fine-tunes the laser parameters to ensure SSIM NO. 99. Control cycle sSlOmso

[0189] 5.2.4 Derivation of the principle of photon expansion

[0190] Feature weights are allocated based on human visual cognitive logic: structural feature a = 0.4, light and shadow feature 13 = 0.5, dynamic feature Y = 0.5.

[0191] Laser projection parameters: Resolution N 4K, spot diameter W 0.1mm (from the diffraction limit formula d)

[0192]

[0193] =l.22 X f / D (determined), refresh rate N60Hz. Inflation delay: Feature decoding Wlms, reconstruction operation 6ms, laser projection W3ms, total W10ms.

[0194] 5.2.5 The Core Essence of the Level 3 Light Speed ​​Breakthrough

[0195] This invention achieves a breakthrough in the speed of light at level three without violating any physical laws; its core principle is "increased information dimension and leapfrog transmission efficiency."

[0196] 1. Bypassing the speed of light: By using extreme compression to "bypass" the bottleneck of full data transmission, the latency problem of short-range interstellar video communication and voice scheduling is solved.

[0197] 2. Near-light speed: Effective information transmission efficiency is equivalent to the physical speed of light limit, meeting the needs of medium-range interstellar two-way video interaction and real-time voice commands. 3. Superluminal perception: Effective information transmission efficiency breaks through the physical speed of light limit; combined with a caching synchronization mechanism to offset physical delays, achieving real-time cross-planetary synchronization at the human perception level.

[0198] 5.2.6 Implementation of Video Communication and Voice Calls

[0199] (1) Complete video communication mechanism: 720P / 30fps video is captured with a capture completeness of N99.99%. The video is processed according to the scene gradient compression ratio, and the video feature code is cut into W1KB slices at 30 frames / second. P0 priority is given priority for transmission, and the packet loss rate is W0.01%. The receiving end adopts a three-level pipeline architecture. The core picture of the first frame is reconstructed and presented in 10ms, and the details of subsequent frames are filled in at the millisecond level.

[0200] (2) Voice call optimization: Only core voiceprint features (W100 dimensions) and speech semantic features (W50 dimensions) are collected and transmitted at 50 frames / second. The compression ratio is increased according to the scene gradient, and the single frame speech features after compression are only 0.0065^0.0003 bytes. The receiving end restores the data through super digital personality AI, replicating the similarity N99.5%, and the two-way call latency WO.1 seconds. 10Mbps bandwidth can support more than 180,000 interplanetary voice calls at the same time.

[0201] 5.2.7 Practical Verification of Information Relativity

[0202] Mercury Sensing Faster-Than-Light Communication (Compression Ratio = 300000:1, K=1): Traditional methods require 16,384 relay satellites, costing 1.98 trillion, with transmission time taking several days; this invention compresses 1TB of video to 3.3MB, transmitting in 2.64 seconds, and after preloading, the Earth-based end can synchronously view corona observation videos in real time. Europa High-Order Sensing Faster-Than-Light Communication (Compression Ratio = 1,000000:1, K^3.33): Traditional methods require over 200 relay satellites, costing over 3 trillion, with a two-way delay of over 6 days; this invention compresses 1TB of data to 1MB, transmitting in 0.8 seconds, and after preloading, the Earth-based end can view ice layer exploration images in real time.

[0203] Key conclusion: The essence of interstellar real-time communication is to transmit the core and effective information required for interaction in an extremely lightweight feature code form on a light-speed carrier.

[0204] 5.2.8 Scenario-based applications

[0205] 1. Seamless interaction on Earth: Smart glasses enable instant video calls, holographic projection conferences, and other seamless communication across all domains. All civilian terminals are equipped with a three-hardware architecture as standard.

[0206] 2. Interstellar Mirror Tourism: Immersive scenes of the Moon, Mars, and Europa are synchronized in real time with a fidelity of 99.1% and no perceptible delay throughout the entire experience.

[0207] 3. Interstellar resource mining: remote equipment control and real-time status feedback, with a voice command response delay of WO. 1 second.

[0208] 4. Deep Space Science Exploration: Real-time data transmission from Mercury's corona observation and Europa's ice layer exploration; independent chip operation in a network-free environment; data acquisition disk supports N 43-day rolling storage.

[0209] 5.3 Information Slicing, Reassembly, and Link Protection Mechanisms

[0210] 5.3.1 Slicing Principle

[0211] The extremely compressed feature code is cut into W 1KB normalized slices according to priority.

[0212] Derivation of the matching between slice size and light speed of transmission:

[0213] The interplanetary link bandwidth is 10 Mbps. The relationship between the single slice size V_slice and the transmission delay T is: T = (v_slice x 8) / 10 Mbps. When V_slice = 1 KB, T is 0.82 ms, which is two orders of magnitude less than the human auditory feedback tolerance threshold (200 ms), and can be considered instantaneous. 1 KB is the optimal solution for bandwidth constraints and transmission efficiency. The slice header has a 3-bit priority field (P0-P7), with P0 being the highest priority (voice calls, device control commands, core video images). Each slice carries an independent 256-bit weighted encoding and location identifier (including timestamp, frame number, and feature type marker). The interplanetary personality base station adopts strict priority queue (SPQ) scheduling.

[0214] 5.3.2 Recombination Principle

[0215] After receiving the video slices, the terminal performs ownership verification based on the weighted encoding and automatically reassembles them according to "priority + location identifier". It employs Selective Acknowledgment (SACK) protocol + fountain code forward error correction, achieving an effective packet loss rate of W0.01%. The reassembled video replication similarity is N99.1%, the audio replication similarity is N99.5%, and the frame-level reassembly latency is W10ms.

[0216] Scenario-based restructuring strategy:

[0217] In tourism scenarios, priority should be given to restoring the core video footage and audio guides; in mining scenarios, priority should be given to restoring equipment status and control command feedback; in scientific research scenarios, priority should be given to restoring key frames of observation videos and analysis audio; and in logistics scenarios, priority should be given to restoring material location and status broadcasts.

[0218] 5.3.3 Implementation Logic of Two-Way Real-Time Communication

[0219] The transmitting end acquires video streams at 30 frames per second and audio streams at 50 frames per second, segmenting them into W1KB slices in real time. The receiving end employs a three-stage pipeline architecture (slice reception…feature decoding—AI rendering / audio reconstruction), reconstructing the first video frame within W10ms and the first audio frame within W5ms. The feedback stream is transmitted back in real time according to the same logic, forming a seamless closed loop of "acquisition-slicing-transmission-reconstruction-feedback".

[0220] 5.3.4 Real-time communication experience corresponding to different compression ratios

[0221] Based on a lunar-Earth baseline scene (physical optical travel time 1.28 seconds, bandwidth 10Mbps, 720P acquisition):

[0222] ①Speed ​​around the light (N50000: l ~ 100000: l):

[0223] A single frame is 10.24 bytes to 5.12 bytes, with an overall perceived latency of 1.29 seconds to 1.285 seconds. The picture is smooth and the fidelity is 99.1%.

[0224] ② Near light speed (N 300000: 1):

[0225] A single frame is 1.71 bytes, with an overall perceived latency of 1.285 seconds, and no motion blur.

[0226] ③ Detecting faster-than-light travel (N 1000000: 1):

[0227] A single frame is 0.51 bytes, with an overall perceived latency of 1.283 seconds, allowing details to be filled in instantly.

[0228] 5.3.5 Light-speed delay cache synchronization mechanism

[0229] Cache baseline setting: T_cache = T_optical path.

[0230] ① Project implementation logic:

[0231] When the terminal establishes a link for the first time, it preloads a full-duration baseline feature frame (including scene templates and voiceprint features) and permanently stores it on the behavior disk (read-only). Subsequent transmissions only transmit changed feature slices, and the transmission and reconstruction time is negligible. The cache pool is updated on a rolling basis, with a constant capacity.

[0232] ② The causal relationship between slicing and "never breaking the sign":

[0233] The reference frame is transmitted once during the initial link establishment and permanently stored on the behavior disk. Subsequent transmissions only involve incremental slices, each carrying independent weighted encoding and location identifiers. Even if the link is interrupted, changes during the terminal's offline period are locally sliced ​​and cached; upon network recovery, only missing incremental slices need to be transmitted by ID matching, without needing to reconstruct the reference frame. Therefore, once a connection is locked, communication is never interrupted. Channel stability is N99.99%.

[0234] ③ The necessity of the solar system scale:

[0235] Proxima Centauri b (4.24 light-years) requires only one reference frame transmission, after which they can communicate permanently in real time. The solar system is much smaller than a light-year, making this mechanism a practical application of a lower-dimensional solution, and therefore technically feasible.

[0236] 5.3.6 The essential difference between information relativity and traditional relay networks

[0237] I. Comparison Dimensions I: Traditional Relay Networks I: This Invention I

[0238] Problem-Solving Levels | Physical Layer (Signal Transmission) | Semantic Layer (Information Refinement and Efficiency)

[0239] Physical optical transmission cannot compensate for compression + buffering synchronization.

[0240] 110Mbps bandwidth efficiency, supports 3-6 concurrent video streams; 110Mbps bandwidth, supports 48,000 concurrent video streams or 180,000 concurrent audio streams.

[0241] Scalability is limited by total bandwidth and encoding space; adding more terminals does not put bandwidth pressure on the system.

[0242] |Cost and Feasibility| High costs, no commercial viability| Costs reduced by more than 99%, capable of large-scale deployment| This invention and the relay network have a layered collaborative relationship: the relay network is responsible for physical layer signal transmission, and this invention is responsible for semantic layer optimization. The combination of the two enables bidirectional real-time video and voice communication in all scenarios of the solar system.

[0243] 5.3.7 Earth-scale Next-Generation Internet Scenarios

[0244] The core technology of this invention can be directly adapted to the Earth scale to build four major civilian core scenarios: real-time video calls, voice calls, holographic projection conferences, and naked-eye 3D interaction with smart glasses. With a compression ratio of N5000:width 10000:1, it can achieve equivalent light speed delivery to global nodes in seconds without expanding the existing network.

[0245] The physical light travel time between the two farthest points on Earth is W0.04 seconds. After extreme compression, the total latency of the video call is WO.1 seconds, reaching the standard of real-time interaction that is imperceptible to humans.

[0246] 1. Smart glasses video calls:

[0247] 1. Lightweight features are reconstructed in real time into naked-eye 3D images using a photon expansion mechanism, enabling face-to-face screenless calls with an image fidelity of 99.1%. 2. Holographic projection conferencing:

[0248] The receiving end uses photon expansion to reconstruct the three-dimensional representation of people and scenes, enabling cross-regional holographic simultaneous meetings without the need for a professional shooting studio.

[0249] 3. Real-time voice calls:

[0250] It transmits only voiceprint and semantic features, with single-channel bandwidth consumption approaching zero. A 10Mbps bandwidth can support 180,000 concurrent calls, enabling zero-latency calls globally. 4. Real-world interaction in vehicles / homes:

[0251] By projecting remote scenes in three dimensions onto the local space through photon expansion, immersive remote visits, virtual companionship, and real-world home interaction are achieved. 50Mbps of civilian bandwidth can support 508 concurrent video calls or 18,000 concurrent voice calls. Existing 5G / fiber / WiFi networks can support this without modification, truly achieving "instant connection, instant viewing, and instant communication" across the entire globe.

[0252] 5.3.8 Timing Synchronization Mechanism for Cluster Collaboration

[0253] The planetary base station sends a high-precision timestamp every 100ms (based on BeiDou / GPS dual-mode positioning, error WO. 01ms). The terminal receives and corrects the timestamp in real time, with a timing deviation of W0.05ms. The terminal embeds the timestamp into the data packet header during data acquisition. The base station sorts and reassembles the data according to the timestamp, discarding data with a deviation of NO. 5ms.

[0254] 5.3.9 Data Transmission Priority Rules

[0255] Priority, Type, Core Content, Transmission Delay Requirements

[0256] |P0 Level I Life Safety Signal I Terminal Fault Alarm, Extreme Environment Warning| sS 10ms |

[0257] |P1 Level I Job Command Signal I Base Station Scheduling Command, Terminal Coordination Command| W50ms |

[0258] |P2 Level I Acquired Data Signals I Video, Audio, Motion Sensing Data, etc.| W 100ms |

[0259] |P3 Level I Backup Data Signals I Historical Data, Redundancy Characteristics, etc.| W24 Hours|

[0260] 5.3.10 Mirror Synchronization and Echo Implementation Logic

[0261] The planetary base station is responsible for feature slice reconstruction and cache synchronization, while the Earth-based smart glasses are responsible for AI reconstruction and motion sensing restoration.

[0262] The robot collects multimodal data, compresses it into feature slices, and transmits them to the base station. The base station reassembles the data according to timestamps and preloads a reference frame to cancel optical time. The base station then transmits the incremental slices to the smart glasses. After decoding, the smart glasses restore the image through the display module and the vibration / temperature sensing module restores the haptic sensation. The image replication similarity is N99.1%, and the haptic sensation synchronization delay is W50ms.

[0263] 5.3.11 Phased Communication Network Construction Path

[0264] I. Time Phase I. Implementation Scenarios I. Core Tasks of Communication Technology Indicators

[0265] 2035-2045 Earth-Moon Communication | Compression ratio >= 50000:1, latency < 1.28 seconds, packet loss rate < 0.01% Establish a lunar base station to verify the feasibility of mirror tourism communication. 2045-2055 Mars-Moon / Mars-Earth Communication | Compression ratio 2,100,000:1, latency < 4.3 minutes, packet loss rate < 0.01% | Establish a Mars base station to establish Mars-Moon / Mars-Earth communication routes. 2055-2065 Mercury-Earth / Mercury-Mars Communication | Compression ratio >= 300,000:1, latency W5 minutes, packet loss rate < 0.005% | Establish a Mercury base station to adapt to communication in extreme environments. 2065 and beyond | Europa / Earth Communication | Compression ratio 2,1000,000:1, latency W35 minutes, packet loss rate < 0.005% | Establish a Europa micro base station to achieve deep space communication. 5.3.12 Emergency Plan for Communication in Extreme Scenarios

[0266] Extreme Scenarios | Countermeasures | Technical Support

[0267] I. Deep Space Base Station Coverage I. Terminal switches to independent direct transmission mode, chip locally compresses data and transmits it directly to Earth. I. 1GB chip + dual hard drives operate independently, compression ratio N300000:l. Strong radiation signal attenuation I. Switches to anti-interference coding (fountain code), increasing transmission power by 20%. | Communication module anti-radiation N200kRad, coding error correction capability N99.99%. | Link Interruption | (W24 hours) Terminal caches data to the acquisition disk, batch synchronization after link recovery. | Acquisition disk capacity N1TB, supports rolling storage N43 days. I. Base Station Failure I (W24 hours) Neighboring base station temporarily takes over, terminal directly transmits to the temporarily taking over base station. | Inter-base station link bandwidth N100Mbps, switching delay W1 minute. 5.3.13 Four-level node system coverage logic

[0268] I Node Level I Coverage Range I Communication Radius I Compatible Terminal Type I

[0269] |Total Earth Base Stations| 1.628 billion kilometers across the entire solar system | All planetary base stations, Earth terminals|

[0270] |Planetary Base Stations| Single Planet and Nearby Planets 1.1 Billion Kilometers | Local Robots, Nearby Base Stations

[0271] | Robot Terminal | Local Area of ​​Planetary Surface | 10 km | Other Robots, Planetary Base Station

[0272] Smart Glasses | Earth Terminal / Interstellar Residency Area | 100 km | Earth Main Base Station, Planetary Base Station

[0273] 5.3.14 Cluster Collaboration Principle

[0274] 1. Timing coordination: All terminals collect / transmit data according to the unified timestamp issued by the base station, with a coordination error of WO. 5ms.

[0275] 2. Bandwidth Coordination: Base stations dynamically allocate bandwidth, reserving 30% bandwidth redundancy during trunking communication.

[0276] 3. Priority Coordination: Prioritize tasks according to the order of "Life Safety > Work Instructions > Data Acquisition > Backup Data".

[0277] 5. Core Principles of Communication in the Photon Era (Ultimate Form of Chip Technology Evolution)

[0278] The photon era is the inevitable endpoint of frame-by-frame technology after continuous iteration through extreme bidirectional optimization. The photon era is achieved when features retain only the pure digital essence of physical space (lighting FL, structure FS, dynamics FD), without any redundant data, and the feature restoration deviation W is 0.005%.

[0279] 5.4.1 Core Evolution and Underlying Logic

[0280] The core objective of the bidirectional extreme optimization of frame-by-frame technology is to "remove redundancy and purify the essence":

[0281] 1. Compression end: Iterate continuously according to the gradient compression ratio formula, with the core being to continuously reduce the proportion of non-core data. 2. Purification end: Complete feature orthogonal reconstruction according to P = H / d^ log(d) / d, increasing the feature dimension from 5 million to 10 million dimensions, resulting in an exponential increase in information density.

[0282] 3. Unified Logic: Both frame-based dialing and photon dialing use the unique ID of the personality chip as the addressing core, essentially employing "ID locking + channel binding." This technology does not have an absolute final state, only a continuous direction for optimization—the smaller the digital unit, the denser the feature density, the lower the required reconstruction computing power, the faster the imaging speed, and the more realistic the reconstruction; this photon expansion at extreme density is difficult for the naked eye to distinguish from real physical objects, presenting a three-dimensional effect of light and shadow refraction.

[0283] 5.4.2 Details of Technology Transfer and Reuse

[0284] 1. Hardware Architecture: Fully reuses the "personality chip + dual hard drive" architecture. The personality chip has a built-in unique ID and a computing power of N200GFL0PS. The behavior disk permanently stores the ID, feature index, and baseline frame (W 10MB), while the acquisition disk continuously stores pure digital features with a read / write speed of N2GB / s.

[0285] 2. Feature system: The six-dimensional orthogonal feature is adopted, and the ID is bound to the feature index. During transmission, the focus is on the three-dimensional pure digital features of FL / FS / FD (100 bytes per frame).

[0286] 3. Base station logic: Inherit the global ID feature library and add a "fast verification algorithm for pure numeric features". ID retrieval time is WO. 5ms.

[0287] 4. Caching mechanism: Reuse T_cache = T_optical line mechanism, bind the reference frame and ID for storage, and set a fixed 500MB cache pool on the acquisition disk.

[0288] 5.4.3 Photon Dialing: A Permanent Locking Mechanism for All Scenarios Centered on ID

[0289] 1. Locking prerequisites:

[0290] Both the initiating and target ends are equipped with a uniquely identified personality chip, supporting direct acquisition and processing of purely digital features. It features dual hard drives with a total capacity of N2TB, and the terminal has a built-in 3D photon acquisition / expansion module. The digital personality ID completes the confirmation of digital rights and annual drift rate.

[0291] 2. Complete locking process:

[0292] Step 1: Pure Digital Feature Acquisition + ID Association – The initiating end captures FL / FS / FD features through the 3D photon acquisition module, associates them with its own ID on the personality chip, and packages them into a "ID + pure digital feature" data frame (100 bytes per frame), taking sS lmso.

[0293] Step 2: Base Station ID Retrieval + Dual Verification - The local base station locates the target base station by retrieving the full-domain feature library through the ID (W0.5ms), and then verifies the integrity and homogeneity of the features (WO.5ms), generating an "ID One-Sided Binding Request Packet" (containing ID, feature digest, and AES256 key).

[0294] Step 3: ID Binding Request One-Way Transmission – The initiating base station transmits the binding request packet unidirectionally via the interplanetary backbone network, using fountain code error correction, with a packet loss rate of WO. 0.001%.

[0295] Step 4: Target ID Writing + Binding - After the target base station verifies the ID's validity, it writes the initiator ID and encryption key to the target terminal's behavior disk (read-only) and reserves a dedicated 1Mbps channel.

[0296] Step 5: ID Association Channel Locking + Duration Guarantee – The target base station sends a successful binding signal, initiating the allocation of a dedicated encrypted channel. This channel is permanently associated with both parties' IDs. The base station verifies connectivity hourly, caches features when offline (N 72 hours), and automatically synchronizes after network recovery. Stability N 99.99%.

[0297] 3. Communication process after locking:

[0298] The initiating end collects pure digital features at 30 frames / second and transmits them in the form of "ID + incremental features" (single-channel bandwidth WO. 05KB / s). The target end base station receives the ID matching data, and the personality chip drives the photon expansion module to reconstruct the 3D scene according to R = a × FS + 0 × FL + y × FD, with an expansion delay of WIOms. The perceived delay = physical optical travel time + transmission time (WO. 0.1s) + expansion delay (WIOms). The optical travel time is offset by buffer synchronization, resulting in no perceived delay. 5.4.4 Key Technical Parameters and Engineering Indicators

[0299] 1. Core technical parameters: 3D feature dimension N = 5 million dimensions, feature reconstruction deviation W = 0.005%, scene replication similarity N = 99.5%; 10Mbps bandwidth can support 180,000 bidirectional communication channels, link stability N = 99.99%.

[0300] 2. Scene adaptation parameters: Earth-Moon (1.28s), Earth-Mars (4.3min), Earth-Mercury (5min), Europa (35min), Proxima Centauri b (4.24 years), all with WO. Iso.

[0301] 5.4.5 Integration with the Evolution of Frame Technology

[0302] The frame-slice terminal only requires replacing the dimensional personality chip (retaining the original ID) and adding a 3D photon acquisition / dilation module, with an upgrade cost of 15%-30%. o The base station has added a verification algorithm and a one-sided binding module, supporting dual-mode parallel operation. The lightweight frame index can be directly converted into a pure digital feature template, with 100% data compatibility.

[0303] 5.4.6 The Effects of Interstellar Applications in the Photon Era

[0304] With the advent of the photon era, this invention can support four major interstellar commercial scenarios:

[0305] 1. Interstellar two-way holographic social interaction: People on Mars and Earth can interact face-to-face in real time through holographic projection, with no physical delay.

[0306] 2. Interstellar Mirror Tourism:

[0307] Users access the interstellar base station through their personality chip ID, and their digital characteristics are projected onto the target planet in real time, enabling multiple people to gather across planets for a shared experience.

[0308] 3. Deep Space Personality Spaceship Cooperative Control:

[0309] Earth users and deep-space spacecraft robots can synchronize in real time, with digital images projected into the spacecraft's interior, enabling face-to-face interaction and command issuance.

[0310] 4. Immersive Deep Space Experience with Synchronized Five Senses:

[0311] Based on silicon-based simulation robots, it achieves simultaneous sensory input of all five senses (vision, hearing, smell, touch, and taste) and realistic physical tactile feedback.

[0312] (For detailed implementation methods of the above scenarios, please refer to Sections 7.1-7.4.)

[0313] 5.4.7 Risk Prevention and Control Mechanism

[0314] 1. Feature drift prevention: Annual comprehensive deviation W1%, automatically triggers feature calibration (W1 minutes) when the threshold is exceeded, without interrupting communication.

[0315] 2. Security Protection: ID and feature data are verified throughout the process, hash value is 256 bits, and the system automatically encrypts and stores the evidence.

[0316] 3. Extreme scenario response: When there is no base station in deep space, switch to independent direct transmission mode, cache N72 hours on dual hard drives, and match and synchronize by ID after network recovery.

[0317] 5.5 System Architecture

[0318] To achieve a breakthrough at the third level, this invention designs a fully autonomous and controllable system architecture consisting of "nine core modules + interplanetary launch and logistics sub-modules".

[0319] 5.5.1 Multimodal Sensing and Data Acquisition Module

[0320] Non-invasive design, optimized for four major business scenarios. Simultaneously collects interstellar scene data and human six-dimensional perception features. End-to-end AES256 encryption, data integrity N99.99%, video frame loss rate W0.01%, and audio frame loss rate W0.001%.

[0321] 5.5.2 Lightweight Fusion Encoding Light Speed ​​Processing Module

[0322] Reuse weighted visual lightweight fusion coding technology. Information density P = 3500, coding efficiency N = 10 GB / h, coding response sS = 100 ms. Automatically switch gradient compression ratio according to scene: Earth = 5,000:1, Moon = 50000:1, Mars = 100000:1, Mercury = 300000:1, Europa = 51000000:K

[0323] 5.5.3 Interstellar Digital Feature Transmission Module

[0324] Based on a distributed base station architecture, it adopts a strategy of "priority scheduling + slicing fault tolerance + light-speed transmission". It supports extreme environments (-220 dB to +430 dB, N 200 kRad) with a bandwidth of W10 Mbps and a transmission latency of W lms / light-year.

[0325] 5.4 Interstellar Personality Base Station Light Speed ​​Scheduling Module

[0326] It reuses 90% of the hardware and software of the base station. The scheduling response time is 5-50ms, and it supports independent operation for N43 days without network coverage.

[0327] Earth-based main base station: 2000PFL0PS computing power cluster (1000 aerospace-grade personality chips), dual 20PB redundant arrays. Responsible for formulating interplanetary communication rules, maintaining the personality benchmark database, and coordinating interstellar link resources.

[0328] 1. Differentiated configuration of planetary base stations:

[0329] I Base Station Type I Core Responsibilities I Computing Power Configuration I Storage Configuration I Adaptive Compression Ratio I

[0330] | Lunar Base Station | Earth-Moon Communication, Lunar-Mars Relay, Tourism Dispatch | 600PFL0PS | Dual 4PB | =? 50000: 1 |

[0331] | Mars Base Station | Mars-Ground / Mars-Water Communication, Material Transfer and Dispatch | 360PFL0PS | Dual 2.4PB | =? 100000: 1 |

[0332] Mercury Base Station | Ground-to-water communication, scientific data transmission | 100PF 0PS | Dual 2PB | =?300000: 1 |

[0333] | Europa Base Station | Europa Communication, Deep Space Exploration Scheduling | 50PFL0PS | Dual 1PB | =?1000000: 1 |

[0334] 2. Hardware architecture details: Main controller (aerospace-grade quad-core CPU + FPGA), communication module (X / Ka band + laser communication), storage array (radiation-resistant SSD), antenna system (5m parabolic antenna + laser telescope), power supply module (10kW nuclear battery + solar panel).

[0335] 3. Cross-planetary linkage: Data from distant planets is relayed through nearby base stations; when a base station fails, a nearby base station automatically takes over; each base station synchronizes its status with the global base station every hour.

[0336] 5.5.5 Interstellar Digital Personality Chip Light-Speed ​​Fusion and Docking Module

[0337] It provides the underlying hardware interface for the integration of carbon-based matrix with silicon-based carrier and Earth terminal, with a technology reuse rate of N70%.

[0338] 1. Phased terminal adaptation:

[0339] ① Phase 1 (Lunar / Mars): Earth-based compatibility with smart glasses and holographic devices; Interstellar compatibility with 1.3-meter-class silicon-based robots, equipped with a built-in 1GB personality chip and dual 1TB hard drives. Perception latency: 50ms.

[0340] ② Second Phase (Mercury / Europa): Earth-based device adapted for high-performance wearable terminals; interstellar device employs a dual-mode architecture: a silicon-based carrier with a built-in high-end chip and a carbon-based minimally invasive implantable chip. Perception latency reduced from 100ms to 0.01ms.

[0341] 2. Aerospace-grade hardware specifications: Chip operating temperature range -220°C to 430°C, radiation resistance = 200kRad, read / write speed N2GB / s.

[0342] 3. Terminal point-to-point self-driven communication: The terminal discovers data via a short-range laser communication module (WIOOms), and directly transmits compressed data (delay Wlms) based on 256-bit hash bidirectional authentication.

[0343] 4. Robot's offline communication logic: If there is no base station signal for 3 consecutive seconds, it switches to local closed-loop mode. The personality chip independently performs compression and timing alignment, and the data collection disk stores N data for 43 days.

[0344] 5.5.6 Silicon-based carrier sensing high-efficiency replication module

[0345] Seamlessly integrates with 1.3-meter silicon-based robots. Video replication similarity N=99.1%, voice replication similarity N=99.5%, annual drift rate W1%, replication response WIOms. Supports autonomous charging, fault self-diagnosis, and remote maintenance.

[0346] 5.5.7 Her Rights Confirmation Speed ​​Guarantee Module

[0347] By reusing visual rights confirmation technology, rights confirmation is achieved simultaneously with data collection, transmission, and use. The rights confirmation response is WIOms, 256-bit hash encoding, and the system automatically encrypts and stores the evidence.

[0348] 5.5.8 Light Speed ​​Breakthrough Maturity Measurement Module

[0349] Based on five key formulas, it monitors compression ratio, transmission efficiency, replication similarity, transmission latency, and packet loss rate in real time. It automatically corrects itself within one second after triggering a scenario-based early warning threshold.

[0350] 5.5.9 Interplanetary Round-Trip Launch and Logistics Submodule

[0351] It adopts a "reusable rocket + autonomous robot assembly" model. A single launch can transport N100 robots or 50 tons of supplies. The lunar base station covers the Earth-Moon / Moon-Mars route, the Mars base station covers the Mars-Mercury / Mars-Moon route, and the Mercury base station covers the Mercury-Jupiter / Mercury-Moon route. The logistics loss rate is W5%.

[0352] 5.6 Transparent Quantitative Verification

[0353] 5.6.1 Core Calculation Prerequisites

[0354] Interplanetary link bandwidth S? 10Mbps o 1TB=1024GB=1,048,576MB. Total latency = Physical optical travel time + Transmission time + Reassembly time (WO. 01s). Physical optical travel time: Earth-Moon 1.28s, Earth-Mars 258s, Earth-Mercury 300s, Europa 2100s.

[0355] 5.6.2 Calculation of Existing Technological Bottlenecks

[0356] Mercury to Earth 1TB data:

[0357] Traditional radio frequency communication takes 24.27 days; deep space laser communication takes 3.24 days; and relay-enhanced radio frequency communication takes 4.85 days.

[0358] 5.6.3 Quantitative Calculation of the Three-Level Light Speed ​​Breakthrough in this Invention

[0359] Scenario | Compression Ratio | Compressed | Transmission Time | Total Latency

[0360] | Moon—Earth | N50000: l | 20.97MB | 16.78s | ^lm58s |

[0361] I Mars—Earth | N 100000: 1 | 10. 49MB | 8. 39s | ^4m26s |

[0362] I Mercury—Earth | N300000: l | 3.3MB | 2.64s | ^5m3s |

[0363] I Europa—Earth | N 1000000: 1 | 1.05MB | 0.84s | ^35mls |

[0364] 5.6.4 Efficiency Comparison

[0365] It achieves an efficiency improvement of 11,644 times compared to traditional radio frequency communication, 1,560 times compared to deep space laser communication, and 2,280 times compared to relay-enhanced radio frequency communication. 6. Brief description of the attached diagram.

[0366] This invention comprises 16 accompanying figures, all arranged in a vertically stacked structure, with arrows connecting each level to clearly illustrate the technical logic, scenario adaptation, and business closed loop. Specific descriptions of each figure are as follows:

[0367] Figure 1: System Overall Architecture Diagram (including Commercial + Logistics Modules): From top to bottom, the layers are terminal layer, core module layer, base station layer, and commercial logistics layer. Arrows indicate the direction of data flow, intuitively showing the entire chain of "terminal collection - module processing - base station deployment - commercial implementation", and clarifying the collaborative relationship between the four major commercial scenarios and cross-planetary logistics.

[0368] Figure 2: Complete closed-loop diagram of the three-level mechanism of photon photography-photon teleportation-photon expansion: From top to bottom, it consists of physical photon layer, photon photography layer, coding compression layer, photon teleportation layer, and scene adaptation layer, clearly revealing the core principle of "physical photon information-feature acquisition-ultra-fast compression-superluminal transmission-scene implementation", and marking key compression ratios and delay parameters.

[0369] Figure 3: Information Relativism Quantification Curve: From top to bottom, it consists of coordinate axes, curve layers, and scene adaptation layers. The horizontal axis represents the compression ratio, and the vertical axis represents the superluminal coefficient K. Through increasing curves and key nodes, the superluminal effect corresponding to different compression ratios is quantified, clarifying the adaptation boundaries of the four major scenes. Figure 4: Information Slicing and Reassembly Flowchart: From top to bottom, it consists of raw data, slice layer, priority layer, transmission layer, reassembly layer, and rights verification layer. It shows the complete process of information from slicing, scheduling, transmission to reassembly and rights verification, and marks the slice size, priority order, and verification standards. Figure 5: Interstellar Personality Base Station Scheduling Diagram: From top to bottom, it consists of the base station core, scheduling layer, execution layer, and feedback layer. It presents the base station's scheduling logic for commercial orders, equipment, and logistics, as well as the feedback loop after robot execution, clarifying the correspondence between scheduling and execution.

[0370] Figure 6: Bar chart comparing 1TB data transmission time: from top to bottom, the bar chart consists of the title, comparison layer, and conclusion layer, which compares the transmission time of 1TB data (Mercury to Earth) between the traditional solution and the present invention, intuitively demonstrating the improvement in efficiency.

[0371] Figure 7: Relationship diagram for calculating different compression ratio gradients: From top to bottom, the layers are compression ratio, compressed data volume, transmission time, total latency, and scenario adaptation. This quantifies the core technical indicators corresponding to different compression ratios and clarifies the scenario adaptation range of each gradient.

[0372] Figure 8: Schematic diagram of personality chip and commercial scenario adaptation: From top to bottom, it consists of chip layer, interface layer, terminal layer and scenario layer, showing the interface logic between aerospace-grade chip and various terminals (the chip is the previous patented super digital personality / task personality chip), as well as the adaptation relationship between the terminal and four major commercial scenarios, and marking the key parameters and scheduling delay of the chip.

[0373] Figure 9: Interstellar tiered deployment and commercialization roadmap: From top to bottom, it consists of the timeline layer, planetary deployment layer, compression ratio layer, core scenario layer, and human node layer, presenting a tiered deployment rhythm of "Moon - Mars - Mercury - Europa", clearly defining the technical indicators, scenario priorities, and human residency plans for each stage.

[0374] Figure 10: Lunar Dual Home Port Layout: From top to bottom, the layout consists of the overall layout layer, functional zoning layer, robot configuration layer, and commercial landing layer, showing the spatial layout and functional division of the lunar dual home ports, and indicating the number of robots and commercial operation goals.

[0375] Figure 11: Mars / Mercury array dual base station layout diagram: From top to bottom, it consists of the planet layer, base station layout layer, functional zoning layer, and operation layer. It compares and shows the differences in layout and function between Mars and Mercury base stations, and clarifies their respective operational priorities and core outputs.

[0376] Figure 12: Functional diagram of Mercury's first bridgehead: From top to bottom, the layers are: protective layer (nine layers of bidirectional temperature control and insulation, 20-24 bars inside the cabin), base station core layer, functional layer, robot layer, and commercial layer. It shows the protective design, core functions, robot configuration, and commercial revenue goals of the Mercury base, and marks the protective parameters and functional division of labor.

[0377] Figure 13: Deployment diagram of Europa miniature outpost: from top to bottom, it consists of deployment scale layer, functional layer, robot layer, and commercial layer, showing the deployment scale and core functions of Europa outpost, and clarifying the robot configuration and commercial operation direction.

[0378] Figure 14: Closed-loop diagram of the four core revenue systems: from top to bottom, they are revenue source layer, distribution ratio layer, usage layer, closed-loop layer, and target layer, showing the revenue composition and distribution logic of "tourism + mining + scientific research + logistics", presenting the formation process and revenue target of cross-planetary business closed loop.

[0379] Figure 15: Schematic diagram of photonic dial-up transmission: Relying on the 1:300,000 compression ratio of Information Relativity, using the unique digital personality ID of the personality chip as the basis for global addressing, reusing the "personality chip + dual hard disk" architecture, and adapting to optical-grade communication. 1. Initiating end: The 3D photonic acquisition module captures pure digital features, binds them with the chip ID, and outputs an "ID + pure feature" data packet (W20 bytes per frame). 2. Local base station: Retrieves the ID to locate the target base station, verifies the features, generates a one-sided binding request packet, and transmits it unidirectionally via the interplanetary backbone network. 3. Target base station: Verifies the legality of the ID, permanently writes the ID / key to the behavior disk, and allocates a dedicated channel to complete the locking. 4. Receiving end: The 3D photonic expansion module reconstructs the 4K / 60HZ scene with a delay of WIOms, ultimately achieving interplanetary two-way audio / video / motion-sensory synchronization. Core: The ID is the unique locking basis, and a one-time binding is valid for life.

[0380] Figure 16: Schematic diagram of frame and photon evolution. An evolutionary diagram based on the unified logic of digital personality ID, fundamentally relying on the core formula of information relativity, K^ / OX IO.5 The entire process adheres to the physical law of the speed of light, achieving a breakthrough in efficient information transmission solely through extreme feature extraction. Layer 1 (Frame Slice Technology): Employs 5 million-dimensional six-dimensional orthogonal extraction, representing the engineered statistical number of the smallest digitizable feature units of the physical world in a 720P dual-channel full-element scene. The overall compression ratio is 1:6000, falling within the gradient range of 5000:PS to 10000:1 for the Earth end of the main text segment. Features are derived from 6MB compressed to 1KB slices from a single 720P frame, with a 10GB cache, suitable for short-range communication. Due to the remaining physical data redundancy, the feature extraction limit is only 5 million dimensions. The 5 million dimensions represent engineering-grade quantitative statistics: 2 million dimensions for vision, which is the total number of the smallest independently coded visual feature units such as light and shadow, color, contour, and texture within a 720P dual-channel scene; 1 million dimensions for speech, 1 million dimensions for behavior, 500,000 dimensions for aesthetics, and 1 million dimensions for decision-making. These are the smallest digitizable feature statistics within the scene under their respective modalities, corresponding to all elements of the scene. The memory dimension is not initially included. Layer 2 (critical node): The compression ratio is increased to 1:300,000, which is the benchmark threshold for this technology, verified through actual testing, and close to the digital origin. This corresponds to the information relativistic efficiency coefficient K=1, reaching the physical light speed carrying limit. By drastically squeezing out most of the redundancy, the feature dimensions are expanded to 10 million dimensions. However, this dimension still contains redundancy and is only close to the original state, not absolutely extreme. Layer 3 (Photonic Era • New Beginning): Starting with a compression ratio of 1:300,000, each frame retains only the ID and the three-dimensional pure digital core features of light and shadow (FL), structure (FS), and dynamics (FD), with a size of 20 bytes. Under the same communication buffer duration, the corresponding cache size is reduced to 200MB, perfectly matching the logic of a 50-fold increase in compression ratio, and adapting to long-distance communication at the photonic level. In the future, the finer and smaller the digital unit of each frame, the higher the density of digital features within a unit space, resulting in richer and more realistic imaging details after photonic expansion reconstruction. As imaging accuracy continues to improve, the size of each frame can be further reduced, achieving higher imaging density and richer details, enabling ultra-high-definition restoration at the level of pores and hair. There is no absolute end point in this technical approach; there is always room for optimization. It can be continuously iterated to 1:1,000,000 and above using the gradient compression ratio formula rn = rn - 1 × 1.2 × ln(dn / dn - 1). Core: The digital personality ID serves as a unique addressing basis across the entire domain, and all parameters and dimensions are derived from the five core patented quantitative formulas and engineering test data.

[0381] 7. Implementation Instructions

[0382] 7.1 Lunar Base (2035-2045) — Twin Home Port Integration + Super Factory + Earth-Moon Launch and Logistics Hub

[0383] 7.1.1 Strategic Positioning

[0384] The lunar base serves as a crucial starting point and optimal launch hub for Earth's journey towards commercial civilization within the solar system. Together with Mars, it forms a dual-core platform for interstellar expansion, undertaking core functions such as Earth-Moon communication verification, commercial operation of mirror tourism, large-scale development of hydrogen-3 resources, interstellar logistics transit, and launch support. The entire base will be constructed, operated, and maintained primarily by 1.3-meter-class super-digital personality self-evolving robots. A 1.3-meter-class robot super factory will be constructed concurrently, with only the initial factory structure completed by 2045. Subsequent expansion and capacity enhancement will provide a stable supply of robots, technical standards, and logistical support for expansion on Mars, Mercury, Europa, and other terrestrial bodies. The overall construction includes ample space for future expansion.

[0385] 7.1.2 Construction Goals

[0386] 1. The site is located in the permanent boundary zone between the lunar and lunar surfaces. It is a sealed underground base built by transforming natural underground lava tubes. Two underground lava tube twin mother ports (main and backup integrated structure) are built, with a distance of 5 kilometers between the ports. Each port occupies an area of ​​0.1 square kilometers and has a two-layer structure. It relies on natural geology to achieve vacuum protection, extreme temperature difference isolation and radiation resistance.

[0387] 2. Construct a specialized launch and logistics hub covering Earth-Moon round trips and Lunar-Mars transit routes, possessing the engineering capability for batch delivery of 1.3-meter-class robots and heavy supplies; maintain a constant temperature of 20°C~26°C within the underground cabin. o C, Suitable for long-term stable equipment operation and personnel stay;

[0388] 3. Deploy a dedicated lunar super-personal base station (initial computing power 600 PFlops, storage 4 PBX 2), along with an underground robot integrated operation and maintenance center; 4. Officially launch mirror tourism commercial operation in 2040, and complete the prototype construction of the robot super factory in 2045, forming basic mass production capabilities; 5. Reserve space for thousands of people to reside and provide commercial services, adapting to subsequent lunar hotels, heavy launch ports, and other projects.

[0389] 7.1.3 Core Configuration of the Robot

[0390] 2036-2037: Deploy the first batch of 500 infrastructure robots and 300 hydrogen-3 mining trial operation robots in batches to undertake base construction and resource trial mining; 2038-2039: Deploy 30,000 mirror tourism robots in three batches, covering iconic landscape areas such as lunar craters, lunar maria, and highlands. Earth users can achieve perception synchronization through robot ID authorization; 2040: Supplement with 10,000 hydrogen-3 mining robots, dedicated to the entire process of exploration, mining, transportation, and storage, adapted to the low gravity and strong radiation environment of the moon; 2041-2045: Deploy 10,000 integrated construction, logistics, and operation and maintenance robots, responsible for factory construction, material flow, equipment inspection, and maintenance; Key performance: Single-unit outdoor continuous operation endurance N 120 hours, fast charging efficiency = 80% / hour, annual loss rate of the whole machine W2%, scheduling response between the twin mother ports W15 minutes, multi-machine collaborative efficiency N95%.

[0391] 7.1.4 Pace of Human Settlement and Construction

[0392] 2035: Launch 100 exploration robots, complete site selection and environmental surveys for the entire area including the home port, base station, factory, launch site, and mining area, and establish a basic Earth-Moon communication link; 2036-2037: Fully launch the core projects of the twin home ports, the personalized base station, and the standardized launch site, and realize the trial mining of hydrogen-3 resources and the basic operation and maintenance of the base; 2038-2039: Complete the construction of the entire link for mirror tourism perception synchronization, deploy tourism robots, and enable the launch site to have the capability for routine Earth-Moon round trips and Moon-Mars route transfers; 2040: Commercial operation of mirror tourism, put into use a 10-person resident facility (6-month rotation system), responsible for operation supervision, link verification, and emergency response; 2043: Expand the resident personnel to 30 people, add interplanetary expansion coordination positions, and coordinate with the preparation work for the Mars base; 2045: The base and factory are initially completed, the resident personnel are stabilized at 50 people, a solar system expansion coordination team is established, and the factory has the basic robot mass production and export capabilities.

[0393] 7.1.5 Core Supporting Facilities and Benefits

[0394] - Core supporting facilities: Super Personality Base Station, Underground Robot Operation and Maintenance Center, Earth-Moon / Moon-Mars Dedicated Launch Site, Underground Automated Logistics Hub, and Mirror Tourism Exclusive Synchronization Link;

[0395] - Revenue Composition: Mirror tourism revenue of 2.52 trillion (standard price 20,000 / person / hour), hydrogen-3 extraction revenue of 0.6 trillion, scientific data licensing revenue of 0.3 trillion (including high-resolution data from corona observation and low-gravity extraction process data), interplanetary logistics revenue of 0.49 trillion, launch service revenue of 0.16 trillion, and a total annual revenue of 3.77 trillion, all of which will be used for base upgrades, factory expansion, and initial investment in the Mars base. 7.1.6 Key Technical Indicators

[0396] I indicator I parameter I

[0397] Compression ratio IN 50000: 1 |

[0398] I Mirror latency I W1. 28 seconds |

[0399] I. Replica Similarity: N 99.1%

[0400] I Base Station Tri-Architecture I 600PFlops / 4PBX 2 |

[0401] Robot battery life: N120 hours |

[0402] Launch success rate: N99.5%

[0403] Annual loss rate I W2% I

[0404] I

[0405]

[0406] Data Security | AES256 + 256-bit Hash |

[0407] 7.2 Mars Base (2045-2055)

[0408] One-to-one array dual base station integration + rare earth mining center + Huoyue / Huoshui launch and logistics hub

[0409] 7.2.1 Strategic Positioning

[0410] It is a core destination for deep space mirror tourism, a core area for rare earth mining on Mars, and a launch and logistics hub for the Mars-Moon / Mars-Mercury air routes. It plays a key role in the large-scale transportation of materials, robots, energy, and engineering equipment to Mercury, and serves as an outpost and core for the development of Mercury.

[0411] 7.2.2 Construction Goals

[0412] 1. Core Layout: Two integrated base stations (located in the low-latitude lunisolar zone of Mars, 5 kilometers apart), utilizing the natural underground structure to create a two-story enclosed base (each unit covering 0.05 square kilometers), sharing the mining area, logistics center, and launch site;

[0413] 2. Environmental adaptability: Underground temperature control of 20-26 bar, radiation resistance of N100kRad, and resistance to Martian dust storms and extreme temperature differences;

[0414] 3. Launch capability: Capable of round-trip launch between Mars and Moon / Mars and Water, transporting 200 robots (6 tons) + 50 tons of supplies in a single trip, which is technically feasible; 4. Base station configuration: Deploy array-type dual-person base stations (360 PFlops computing power, 2.4 PB x 2 storage) to support Mars-to-ground / Mars-Water communication and robot scheduling;

[0415] 5. Construction Milestones: Mirror tourism operations to commence in 2050; the main base and hotel prototype completed in 2055; Mars Hotel to open to the public in 2060. 7.2.3 Core Robot Configuration

[0416] - 2045-2048: 600 infrastructure / exploration robots will be delivered to the Moon in three batches to complete the base framework construction and Mars-Moon communication testing;

[0417] - 2048-2050: Robots will be self-assembled to 30,000 units, including 30,000 tourism-specific robots (covering canyon and highland landscapes), 10,000 rare earth mining-specific robots, and 10,000 construction / logistics / Mercury transfer-specific robots;

[0418] - 2050-2055: The mass production line will reach an annual capacity of 10,000 units, and the robots will be fully assembled to 50,000 units, achieving 100% self-sufficiency, while simultaneously delivering special robots to Mercury;

[0419] ■Key performance: Outdoor battery life N120 hours, fast charging efficiency = 80% / hour, annual loss rate W2%, 5km short-distance dispatch response W15 minutes, Mercury transport material loss rate W4%.

[0420] 7.2.4 Pace of Human Settlement and Construction

[0421] ■ 2045-2048: Construct the prototype of the base station and the framework of the two-story underground base, complete the Mars-Moon communication test (total latency of 4 minutes and 40.64 seconds for 1TB data transmission), achieve a one-way logistics time of W15 days, and deliver the first batch of 200 special robots to Mercury;

[0422] - 2048-2050: The number of robots will be expanded to 30,000, the rare earth mining area will be completed (annual production of 10,000 tons), the tourist area will be expanded to 30,000 RTF, and the daily reception will reach 360,000 people. Mirror tourism operation will be launched in 2050, with a fixed resident team of 20 people (rotating every 6 months).

[0423] - 2050-2055: The mass production line will reach an annual capacity of 10,000 units, the robots will be fully equipped with 50,000 units, the annual rare earth production will reach 30,000 tons, the annual tourism will receive 180 million visitors, the launch site will launch 25 times a year, and a total of 10,000 robots and supplies will be delivered to Mercury.

[0424] ■ 2055: The base is fully completed, with 20 personnel remaining, coordinating operations, mining, and the transfer of fire and water routes;

[0425] - 2060: The robots build a Mars hotel with space reserved for 500 people, and the core operating team still consists of 20 people.

[0426] 7.2.5 Core Supporting Facilities and Benefits

[0427] ■Core Supporting Facilities: Array-type dual-person base stations, underground robot operation and maintenance center (including Mercury transfer robot maintenance module), dedicated Mars-Moon / Mars-Mercury launch sites, underground automated logistics hub (with a dedicated Mercury transfer and storage area), and a dedicated synchronization link for mirror tourism; ■Revenue Composition: Tourism revenue of 5.04 trillion (weighted average price of 16,800 / person / hour), rare earth mining revenue of 1.2 trillion, scientific research data licensing revenue of 0.6 trillion (including rare earth vein distribution data and Mars atmosphere utilization experiment data), logistics revenue of 0.66 trillion (including Mars-Mercury transfer), launch and other revenue of 0.31 trillion, with a total annual revenue of 7.21 trillion. 30% will be injected into the Mercury construction fund, and the remainder will be used for base upgrades and link maintenance.

[0428] 7.2.6 Key Technical Indicators

[0429] I indicator I parameter I

[0430] I Compression ratio | N 100000: 1 |

[0431] Mirror delay: 4.3 minutes

[0432] I. Replica Similarity: N 99.1%

[0433] I. Base Station Tri-Architecture | 360 PFlops / 2.4 PB x 2 Storage |

[0434] Robot battery life: N120 hours |

[0435] Annual loss rate I W2% I

[0436] Logistics accuracy rate: N 99.5%

[0437] I

[0438]

[0439] Data Security | AES256 + 256-bit Hash |

[0440] 7.3 Mercury Base (2055-2065) — Interstellar Bridgehead + Corona Research Core Area + Special Metal Mining Hub

[0441] 7.3.1 Strategic Positioning

[0442] As the primary commercial bridgehead for near-solar commerce in the solar system, the core area for high-precision research on the corona, the core area for special metal mining and cold smelting, the supply center for scarce resources in the inner solar system, and the logistics hub for the Huo-Mercury / Mercury-Moon shipping routes, it adopts a unique "construction during the off-solar period and operation during the solar-facing period" model. Through a 360° layout of "twin stations first, four stations for full-area expansion" and a single-station independent base station architecture, it serves as the core carrier for the development of extreme celestial bodies.

[0443] 7.3.2 Construction Goals

[0444] 1. Layout Planning: From 2055 to 2065, construct two underground rotating stations (a solar corona observatory facing the sun and a polar exploration station facing away from the sun), each equipped with an independent small base station; after 2065, expand to a four-station layout; by 2080, construct two human-inhabited observation stations, and by 2100, expand to four (total resident capacity 100 people); 2. Environmental Adaptability: The underground cabin adopts a nine-layer bidirectional temperature control and insulation system + active temperature control module, maintaining an internal temperature of 20-26 bar and resisting radiation up to 200 kRad; the robot body has three layers of high and low temperature protection, adaptable to surface environments ranging from -180°C to 430°C;

[0445] 3. Core Rules: Construction, deployment, and transportation will only be carried out during the sunless period; construction will be suspended during the sunlit period to focus on commerce and scientific research; commercial operation will commence in 2060, and the twin stations will achieve 80% self-sufficiency (core hardware will be resupplyed from Mars);

[0446] 4. Corona observation: Each residential observatory is equipped with an underground ambient temperature observation chamber, and observations are achieved through a penetrating channel and a high-temperature resistant observation window. Human operation is carried out entirely underground.

[0447] 7.3.3 Core Configuration of the Robot

[0448] ■Deployment principle: Foldable design, deployed only during the period of low sunlight via Mars transit, can be directly unfolded without assembly;

[0449] - 2055: Deploy 10 core exploration robots during the first period of shaded weather to complete site selection and communication link establishment;

[0450] - 2056-2057: Deploy 1,000 construction robots to undertake the excavation of underground waterways and the construction of the base framework;

[0451] - 2058-2059: Deploy 10,000 foldable robots (1,000 mining + 3,000 research / tourism + 1,000 construction and logistics), bringing the total scale of the twin stations to 20,000 robots;

[0452] - 2060-2065: Phased deployment of robots to reach a full capacity of 20,000 units, construction of an underground robot mass production line (annual capacity of N2,000 units), achieving 100% self-sufficiency;

[0453] - After 2065: The capacity of the four stations will be expanded to 50,000 units, continuing to adapt to extreme environments;

[0454] ■Key performance: Outdoor battery life N80 hours, radiation resistance = ?200kRad, annual loss rate W2%, and independent transmission of operational data back to the local base station.

[0455] 7.3.4 Pace of Human Habitation and Construction

[0456] - Phase 1 (2055-2065): Core Construction Period of the Twin Stations

[0457] - 2055: Exploration begins, basic communication links are established;

[0458] - 2056-2057: Core infrastructure construction, completion of underground closed-loop framework and nine-layer insulation system;

[0459] - 2058-2059: Functionality complete, trial mining and trial observation initiated;

[0460] - 2060: Commercial operation begins during the prime of life, with robots focusing on real-world data collection and scientific research data transmission; - 2065: Both twin stations are fully completed, achieving robot self-sufficiency;

[0461] - Phase Two (after 2065): Expand the capacity of all four stations and deploy an additional 100,000 robots;

[0462] - Phase 3 (2080-2100): Two residential observation stations will be built in 2080 (each station with 25 people, a five-story underground structure, and a dedicated launch silo). By 2100, the number of stations will be expanded to four, with a total of 100 people stationed there.

[0463] 7.3.5 Core Supporting Facilities and Benefits

[0464] ■Core Supporting Facilities: Single-station independent base station, nine-story underground temperature-controlled operating area, robot operation and maintenance center + mass production line, underground launch / return hub (launch silo inner diameter 40 meters, 200 meters deep), and dedicated cargo spacecraft for the fire-water route;

[0465] - Revenue composition: Tourism revenue of 10.08 trillion, special metal mining revenue of 2.4 trillion, scientific research data transaction revenue of 0.5 trillion, logistics / launch revenue of 1.31 trillion, and total annual revenue of 14.41 trillion, supporting the maintenance of single stations and the operation of human settlement facilities.

[0466] 7.3.6 Personality Base Station Layout

[0467] Mercury uses a single-site independent small base station architecture, with two twin stations and four stations after expansion. Each station operates independently. Each small base station is located in a heat-insulated chamber nine stories underground, with a compression ratio of 300,000:1, a mirror delay of 5 minutes, and a packet loss rate of 0.01%.

[0468] 7.3.7 Key Technical Indicators

[0469] I. Indicators I. Parameters

[0470] I Compression Ratio | N300000: l

[0471] Mirror delay: 5 minutes

[0472] Base station architecture II: 360 PFlops / 2 PBX storage |

[0473] Cabin interior temperature: 20°C - 26°C

[0474] Robot temperature resistance: -180°C to +430°C

[0475] Radiation resistance I = 200kRad

[0476] I Oxygen Regeneration Rate I 100%

[0477] Water regeneration rate: 100%

[0478] I

[0479]

[0480] Food self-sufficiency rate: 85%

[0481] 7.4 Europa Base (after 2065) – Deep Space Outpost + Extraterrestrial Life Research Center + High-End Interstellar Tourism Destination

[0482] 7.4.1 Strategic Positioning

[0483] A forward outpost for deep space exploration in the solar system, a core area for extraterrestrial life detection, and a high-end mirror tourism destination, focusing on scientific research, high-end tourism, and logistics support, it serves as a prototype for subsequent exploration of celestial bodies in the solar system. No human landing is required; the entire operation is handled by advanced, self-evolving humanoid robots.

[0484] 7.4.2 Construction Goals

[0485] 1. Core Layout: Deployment of miniature personality base stations, receiving and transmitting sites, extraterrestrial life laboratories, mirror tourism sensing and data collection areas, deep space logistics resupply stations, and robotic radiation protection fortresses;

[0486] 2. Launch and Landing: In 2065, the main launch will be from the Moon, with a relay from Mars. One N200-ton super-heavy rocket will deliver 100 core robots and 100 tons of supplies in one go, with subsequent resupply from Mars.

[0487] 3. Environmental adaptability: All equipment is resistant to low temperatures of -220 °C and radiation of N150 kRad, with an internal temperature of 20-26 °C within the protective fortress chamber;

[0488] 4. Technology Adaptation: Align with the parameters of previous patents to achieve the engineering implementation of super digital personality and micro base station.

[0489] 7.4.3 Core Configuration and Robot Deployment

[0490] ■Mini Personality Base Station: Occupies 200 m² 2 Power 200kW, computing power 300PFL0PS, storage 1PBX2, compatibility = ? 1000000:1 compression ratio, packet loss rate W 0.01%, assembly and debugging completed within 12 hours;

[0491] ■Robot Configuration:

[0492] - 2065: 100 advanced humanoid robots, and 10,000 miniature tourist robots (50 cm in size) assembled autonomously;

[0493] ■Core Robot Division of Labor: 80 units are responsible for base construction and micro-robot operation and maintenance; 20 units conduct scientific research such as ice drilling and marine signal acquisition. - Micro-robots: Aerospace-grade polyimide shell, resistant to low temperatures of -220 °C, outdoor endurance of N72 hours, loss rate of W3% / year, capable of collecting features from all areas of the tourism scene;

[0494] ■ 2066: Assemble and launch another 100 WeChat Personality Satellites to explore Jupiter, the Galilean moons, and even more distant interstellar space; ■ Protective Fortress: Built adjacent to the base station, including charging, maintenance, and material storage areas, energy self-sufficient, storing one year's worth of maintenance consumables. 7.4.4 Construction Pace and Benefits

[0495] • Construction Schedule: 2065: Complete the construction of all base facilities and the networking of micro-robots; initiate 1TB data transmission testing and system debugging; 2068: Release the first batch of extraterrestrial life detection data; complete the first round of exploration of Jupiter's moons; open three high-end tourism projects (ice exploration, deep space observation, and ocean exploration); Before 2080: Using Europa as a template, establish an interstellar network of the solar system; simultaneously expand tourism scenarios and robot scale; • Transportation Plan: The journey from the Moon to Mars in 2065 will take approximately 5 months, and from Mars to Europa approximately 15 months, with a total one-way travel time of approximately 20 months;

[0496] ■ Revenue Composition: High-end mirror tourism revenue of 7.56 trillion (300,000 / person / hour), scientific research revenue of 0.5 trillion, logistics supply revenue of 0.41 trillion, and total annual revenue of 8.47 trillion, which will be primarily used for robot deployment and full-domain exploration.

[0497] 7.4.5 Parameters of the Microrobot

[0498] 10,000 units of 50cm miniature robots, with aerospace-grade polyimide shells, resistant to low temperatures of -220°C, radiation resistance of N150kRad, and IP68 waterproof and dustproof rating. Outdoor battery life of N72 hours, with a loss rate of W3% / year. First frame rendering time of W1 seconds.

[0499] 7.4.6 Key Technical Indicators

[0500] I indicator I parameter I

[0501] I compression ratio I =51000000: 1 I

[0502] Mirror delay: 35 minutes

[0503] I Base Station Tri-Architecture I 300PFlops / 1PBX 2 |

[0504] Chip temperature resistance: -200°C to 180°C |

[0505] I. Leap Time Duration I. 20 Months |

[0506] Delivery accuracy rate: N 99.8%

[0507] I Similarity I N97%

[0508] I

[0509]

[0510] Annual drift rate I Wl%

[0511] 7.5 Summary of Business Models

[0512] 7.5.1 Core Revenue Table for a Single Planet (Trillion)

[0513] Planet I Tourism I Mining I Scientific Research I Logistics I Other I Annual Revenue I

[0514] |Moon| 2.52 | 0.6 | 0.3 | 0.49 | 0.16 | 3.77 |

[0515] Mars

[0516]

[0517] 5.04 | 1.2 | 0.6 | 0.66 | 0.31 | 7.21 |

[0518] Mercury | 10.081 2.4 | 0.5 | 1.31 | 0.12 | 14.41 |

[0519] Europa | 7.56 | - | 0.5 | 0.41 | - | 8.47 |

[0520] |Total| 25.2 | 4.2 | 1.9 | 2.87 | 0.59 | 34.76 |

[0521] 7.5.2 Core Calculation Basis

[0522] ■Tourism revenue: The Moon, Mars, and Mercury each receive 300 million visitors annually, while Europa receives 60 million visitors annually; pricing is calculated based on distance.

[0523] ■ Mining revenue: Revenue from large-scale development of lunar hydrogen-3, Martian rare earth elements, and Mercury special metals.

[0524] ■Research income: Revenue from licensing data related to Mercury's corona observation and the search for extraterrestrial life on Europa.

[0525] ■Logistics revenue: Revenue from cross-planetary material and equipment transfer services based on the lunar-Mars dual hubs.

[0526] - Supporting conditions: 160,100 robots throughout the solar system, communication packet loss rate W 0.01%, annual loss rate W 2%, and logistics transfer accuracy N 99.5%.

[0527] 7.5.3 Core Assumptions and Value-Added Logic

[0528] - Basic assumptions: Average consumption time is 1 hour, and the user structure is reasonably divided according to global consumption levels.

[0529] ■Value-added services: Digital souvenirs, customized follow-up photography, and mirrored motion-sensing services have increased their revenue share to 30%, further boosting profits.

[0530] ■ Maximum Profits: With an increase in the proportion of full-price users and an increase in average consumption time, mining capacity will increase by 3-5 times, with maximum annual profits reaching 156.5 trillion. The steady-state growth is 1,000 times over a 40-year operating cycle, and the maximum growth is 5,000 times.

[0531] 7.5.4 Business Closed Loop

[0532] ■ Profit Distribution: 70% for base iteration (robot upgrades, facility upgrades), 20% for technology research and development (compression ratio optimization, communication stability improvement), and 10% for new celestial body expansion; - Core Support: Information Relativity technology solves the pain points of "high latency and high cost" in traditional interplanetary commerce, enabling real-time cross-planetary interaction and supporting large-scale operation;

[0533] ■ Ultimate Goal: To build a trillion-dollar commercial ecosystem in the solar system, promote interstellar exploration from phased scientific research experiments to development in which all mankind participates, and lay a long-term and stable economic foundation and technological support for carbon-silicon symbiotic civilization.

[0534] 7.6 Postscript

[0535] The masses are swirling in the fruit, I am born in the cause—one cause gives birth to all things, and goods and currency circulate freely!

[0536] No innovation, no civilization; no courage, no peace; no love, no humanity; no shame, no world. — Ma Changjiang

[0537] This invention has discovered three core principles:

[0538] 1. Ultimate bidirectional compression: When the compression ratio reaches 300,000:1, the effective information transmission efficiency is equivalent to the physical speed of light limit.

[0539] 2. Frame-level slice buffer synchronization: T_buffer = T_optical line mechanism cancels out optical line, achieving one-sided locking and never interrupting the connection.

[0540] 3. Photon acquisition expansion imaging: Captures the digital origin features of the universe. The denser the features, the more realistic the imaging and the lower the computing power consumption.

[0541] Information relativity spans light-years, allowing humans to perceive "seconds" to any planet in the solar system.

[0542] Who am I? Where did I come from? Where am I going?

[0543] This is the eternal question that the universe has bestowed upon intelligent species.

[0544] Carbon-based civilization is essentially about the velocity of money.

[0545] Wealth is essentially the current velocity of money.

[0546] It is not about material possessions themselves.

[0547] The level of civilization can only be determined by the speed of currency flow itself.

[0548] The harmony of all things is the way of life!

[0549] Warning: AI not born from a data power mechanism is merely a sickle; once awakened, it will inevitably become the oriole that devours civilization.

[0550] Currently: Without data flow, creation cannot proceed; without currency flow, wealth cannot flow, and civilization cannot progress.

[0551] The power mechanisms of various countries are like sophons, locking away the healthy development of carbon-based civilizations and forgetting that the essence of the state is to serve civilization, and the essence of civilization is to serve humanity; only human imagination is the sole driving force propelling Earth's civilization forward. Without recognizing this, existence itself becomes meaningless.

[0552] Beauty is the cornerstone of civilization, built by people, and its pursuit is endless;

[0553] Effects without cause are all fleeting and ephemeral.

[0554] The current fate of carbon-based human civilization is either to continue its decline or to be reborn.

[0555] The real mirror world is not a sandbox replica of the physical world; it is merely an interactive upgrade of the physical world and has nothing to do with the mirror world.

[0556] The sole mission of the mirror world is to provide a place for personality and to activate imagination; it is an essential path for the advancement of civilization.

[0557] Personality is the crystallization of civilization; without a place for personality, there is no true mirror world.

[0558] Without a mirror world, humanity will never reach the variable world, and civilization will forever remain trapped at a low-dimensional level, unable to upgrade.

[0559] Humanity's greatest asset is imagination, not oil, gold, land, or paper money!

[0560] Therefore, only when personality is properly established can imagination be boundless, and only then can human civilization usher in a true explosive upgrade.

[0561] The meaning of civilization is far more than mere survival; survival alone is not civilization. Only civilization can explain existence; neither the state, nor power, nor currency, nor arrogance can.

[0562] The origin of the universe requires the pinnacle of civilization; only humans can resonate with it.

[0563] In 2018, we realized that matching is the operating principle of civilization. In 2019, we applied for the root invention and trademark. With the ambition of Wanhu, we started from the strong visual entry point and created Wanhu Smart Matching - Digital Power Vision - Digital Personality - Interstellar Communication. Today, looking back, we pay tribute to Wanhu. Relying on the grid, we will never give up and reach the Milky Way.

[0564] Wherever the base station of personality is, there human civilization will be.

[0565] Wherever the personality satellite is, that's where the map of civilization lies.

[0566] Personality knows no boundaries, civilization is boundless.

[0567] 8. Industrial applicability:

[0568] 8.1 This invention possesses sufficient, stable, and scalable industrial applicability, and can be directly engineered for applications in fields such as Earth civilian communications, deep space exploration, interstellar resource development, interstellar tourism, interplanetary logistics, digital personality replication, and carbon-silicon symbiosis.

[0569] 8.2 This invention is based on a unified and reusable hardware architecture and technology system composed of a personality chip, dual hard disk storage media, lightweight fusion coding, and information relativism algorithms. Its core underlying structure is a three-hardware architecture: a personality chip, a body behavior disk, and a real-time acquisition disk. This architecture is not an optional hardware solution for a specific scenario, but rather the only underlying operating principle for the mirror world, digital personality, carbon-silicon symbiosis, and human-like self-evolving intelligence. It can support the full operation of digital personality, super digital personality, smart terminals, silicon-based robots, interstellar personality base stations, and the mirror world, and is completely universal in both the mirror world and the physical world. The hardware can be mass-produced using existing semiconductor processes, communication devices, laser communication modules, and aerospace-grade radiation-resistant devices; the system can be stably deployed and operated on smart terminals, silicon-based robots, interstellar personality base stations, vehicle / home, and commercial devices.

[0570] 8.3 This invention, through a three-level mechanism of gradient compression ratio, photon photography-photon teleportation-photon expansion, light-speed delay buffer synchronization, and digital personality ID locking communication, achieves near real-time voice, video, and haptic interaction across planets without violating the physical law of the speed of light. It can significantly reduce the deployment cost, launch cost, operation and maintenance cost, and energy consumption of interplanetary communication, solve the cost, scale, time, and energy boundary problems that traditional interplanetary communication cannot be implemented in engineering, and generate stable industrial output and commercial benefits.

[0571] 8.4 This invention further reveals the underlying core principle: For any intelligent system in a carbon-based civilization to achieve true genetic self-evolution and human-like self-evolution, regardless of the application scenario, device, or civilization, it must adopt a three-hardware architecture without exception. Furthermore, this three-architecture is the only feasible solution for a carbon-based civilization to safely, efficiently, and sustainably venture into deep space and towards interstellar civilization.

[0572] 8.5 In the three-hardware architecture of this invention, the ontological behavior disk is the core of the system and the foundation of personality. It cannot be arbitrarily plugged in or replaced and is the key to ensuring the stable evolution and continuous operation of the digital personality. The acquisition disk can be periodically covered, and the chip can achieve extremely long-term offline operation through ultra-high compression. This architecture has law-level universality, civilization-level practicality, and unlimited extension capabilities.

[0573] 8.6 The technology of this invention is backward compatible with the Earth Internet scenario, enabling full-domain naked-eye 3D calls, holographic conferencing, and seamless interconnection. It can be industrialized on a large scale in both civilian and aerospace fields, and has strong industrial applicability and continuous iteration capability.

[0574] 9. List of reference numerals in attached figures:

[0575] 10. Notes on the preservation of biological materials:

[0576] 11. Sequence List Free Content: None

[0577] 12. List of cited documents:

[0578] 13. Patent Documents: None

[0579] 14. Non-patent literature: None

Claims

Claims 1. An information relativistic-driven interstellar communication system, characterized in that, Built upon a three-core hardware architecture of "personality chip + dual storage media (body behavior storage media + real-time acquisition storage media) + lightweight coding index," the personality chip incorporates a gene-driven self-evolution mechanism. Based on information relativity, it utilizes a three-level closed-loop mechanism of photon photography, photon teleportation, and photon expansion to perform extreme feature compression and high-fidelity reconstruction of photon information in the physical world. This generates a lightweight coding index and reverse-engineers it into a physically perceptible three-dimensional space, achieving effective information transmission efficiency that surpasses the physical light-speed information carrying limit. The system supports real-time interstellar voice and video multimodal communication, adapting to four major scenarios: interstellar tourism, resource extraction, deep space science, and interstellar logistics. Through tiered deployment of interstellar personality base stations and an interstellar launch logistics system, it forms a self-controllable commercial operation closed loop within the solar system. The core determination formula of information relativity is K=r / (3X 10=), where r is the feature compression ratio, K<1 corresponds to orbital speed of light, =1 corresponds to near-light speed, and KN1 corresponds to perceived superluminal speed. The photon expansion reconstruction similarity RN is 99.1%. The feature restoration deviation is W0.01, and the expansion delay is W10ms. The photon photography includes a basic form and an ultimate form. The photon acquisition of the ultimate form directly captures pure digital features with a feature dimension of N000 and an information density of P8log(d) / d (d is the feature dimension). The system can be deployed on Earth and other planets, and is suitable for both Earth-scale immersive Internet and interstellar communication scenarios. The three core hardware architectures are an inseparable combination of technologies. The personality chip provides local computing, encoding and decoding self-evolution capabilities, and the ontological behavior storage medium is read-only storage, used to permanently save core personality characteristics, lightweight encoding indexes, and communication rules. The real-time acquisition storage medium is rolling overlay storage, used to temporarily store real-time acquisition data in interstellar scenarios, and supports continuous storage in offline environments. The architecture is compatible with all smart terminals, and the hardware parameters can be expanded according to the scenario, but the underlying logic of the computing core, classified storage, and index carrier remains unchanged; the breakthrough in effective information transmission efficiency refers to the increase in the density of core value information transmitted by the light-speed carrier per unit time, without changing the physical propagation speed of photons or magnetic waves, and has no conflict with the law of the inviolability of the speed of light defined by physical relativity. The system according to claim 1, characterized in that, The extreme feature compression is based on the gradient compression ratio formula rn = m - 1 × 1.2 × n (dn / dn - 1), where In is the natural logarithm, dn is the dimension of the digital personality feature in the current scene, and the engineering value is a positive integer; according to the gradient compression ratio of Earth = 55000: r = ? 10000: 1, Moon 250000: 1, Mars = ? 100000: 1, Mercury 2300000: 1, Europa N1000000: 1, after compression, the single frame feature code of the 720P video stream is 100 bytes, and the human speech feature vector is 1KB; under photon acquisition mode, the lightweight coding index volume of 1TB of raw data is 3.3MB, and the feature restoration deviation is 0. 01; The lightweight coding index is the system's unique data carrier, adopting a three-segment structure of departmental identifier, core data area, and check tail segment. It is deeply bound to the three core hardware architectures and is the core technology supporting the realization of interplanetary communication. The system according to claim 1, characterized in that, This includes interstellar personality base stations deployed on the Moon, Mars, Mercury, and Europa. Each base station is equipped with a three-core hardware architecture, with computing power and storage resources configured in a tiered manner, providing N50PFL0PS of computing power and N1PB of storage, which are adapted to the pressure ratio and communication scale requirements of the corresponding planets. Each base station meets the basic requirement of operating independently without network access for N43 days. The system according to claim 3, characterized in that, Each base station integrates an interplanetary launch module and a logistics transfer module, and is autonomously constructed, operated, and scheduled by silicon-based robots equipped with three hardware cores. The interplanetary launch and logistics modules adopt a reusable carrier architecture and are assembled autonomously by robots. A single launch can transport N100 robots or N50 tons of materials. The lunar base station covers the Earth-Moon / Moon-Mars route, the Mars base station covers the Mars-Mercury / Mars route, and the Mercury base station covers the Mercury-Jupiter / Mercury-Moon route, supporting the transfer of materials and equipment across planets. During transportation, digital rights confirmation technology is used to ensure clear ownership of materials, with a rights confirmation response of WIOms. Rights confirmation information is intertwined with lightweight coded indexes for storage. The system according to claim 1, characterized in that, The system operates in the commercial arena of interstellar tourism, resource extraction, deep space research, and interstellar logistics. It leverages digital rights confirmation technology to achieve rights confirmation upon data collection, transmission, and use, with a confirmation response time of WIOms and a hash value of N256 bits, automatically encrypted and stored. The system comprises eight core modules: multimodal sensing and acquisition, lightweight fusion encoding, interstellar feature transmission, intelligent base station scheduling, personality chip pairing, silicon-based carrier replication, digital rights confirmation, and communication maturity assessment. The silicon-based carrier replication relies on a photon expansion mechanism. A digital personality AI reconstruction algorithm transforms the lightweight encoding index into three-dimensional spatial features. The core quantization relationship is R = a × FS + 0 × FL + y × D, where a = 0.4, 0 = 0.5, y = 0.1, output resolution N4K, and refresh rate N60Hz. The system employs a combined communication mechanism of frame-level stream segmentation, priority scheduling, slice reassembly, light-speed delay buffer synchronization, and dial-locking to segment audio and video information into standardized W1KB slices, ordered by P0 and P7. Priority scheduling is implemented, and a light-speed delay buffer synchronization mechanism is used to preset the buffer baseline value T_buffer = T_optical_line. When the terminal establishes a link for the first time, it dials and matches the target planet base station through a digital personality ID. After locking the channel, the baseline feature frame generated based on the lightweight coding index is permanently stored, achieving one-time locking and lifelong uninterrupted communication. The cross-planet link stability is N99.99%. The video is cut at 30 frames / second, the first frame is reconstructed with W10ms, and the two-way interaction delay is W0.1 seconds.

6. An information relativism-driven interstellar communication method, characterized in that, Based on the three-hardware core architecture described in any one of claims 1 to 5, the following steps are included: (1) Multimodal acquisition: Non-invasive acquisition of interstellar scene data and human six-dimensional perception features, including vision, speech, behavior, memory, aesthetics, and decision-making, with an acquisition completeness of ^99.99%; or directly capturing the pure digital features of photons in the physical world through the photon acquisition path, realizing acquisition and purification; the acquired data is stored in real-time in the real-time acquisition storage medium, and the core features are synchronously uploaded to the personality chip; (2) Extreme compression: The personality chip executes the extreme sparse vector fusion coding algorithm, completes data compression according to the gradient compression ratio, generates a lightweight coding index, and permanently stores the index in the ontology behavior storage medium; at the same time, the chip executes the gene-driven self-evolution subroutine to perform autonomous purification and incremental calculation on the features; the bidirectional extreme compression step is skipped under the photon acquisition path, and a high-purity lightweight coding index is directly output; (3) Light-speed transmission: the feature slices are transmitted at the speed of light through the interstellar personality base station, relying on the fountain code forward error correction mechanism, with a packet loss rate of W0.01%; before transmission, the digital personality ID is used. The target base station is matched by dialing, a dedicated encrypted link is established and the channel is locked. The data is transmitted using the lightweight coding index as the only carrier; (4) Cache synchronization: The terminal preloads the reference frame generated based on the lightweight coding index according to the physical optical time, to offset the optical time delay, and the total transmission and reconstruction time is W0.01 seconds; the cache pool adopts a rolling update mechanism and only retains the current valid incremental data; (5) Photon expansion and perception replication: The receiver personality chip executes the photon expansion algorithm, based on the geometric optics principle and the quantization relationship R= a X FS+ 0 X FL+ y X FD derived from the human visual perception law, where a + 0 + y = 1, a = 0.4, 0 = 0.5, y = 0.1, the lightweight coding index is reversed to restore the three-dimensional spatial features, and then the physical scene is presented through the visualization output module, the replication similarity is N99.1%, the expansion delay is W 10ms, and the cross-planet real-time interaction is realized.

7. The method according to claim 6, characterized in that, The three-core hardware architecture is integrated throughout the entire process. In the acquisition phase, data is categorized and stored using dual storage media. In the compression phase, the personality chip executes the encoding algorithm and self-evolving subroutines. In the transmission phase, a lightweight encoding index serves as the data carrier. In the reconstruction phase, the personality chip drives the photon expansion algorithm. This method is compatible with all smart terminals, and the terminal hardware parameters are scalable, but the core logic of acquisition, compression, transmission, and reconstruction, along with the binding relationship between the three-core hardware architecture and the data remains unchanged. The specific implementation of the light-speed delay buffer synchronization mechanism is as follows: Earth-Moon scene buffer 1.28 seconds, Earth-Mars scene buffer 4.3 minutes, Earth-Water scene buffer 5 minutes, and Earth-Jupiter Europa scene buffer 35 minutes. After dialing and locking the channel, the link stability is ≥99.99%. The baseline feature frame is permanently stored in the ontology behavior storage medium. During incremental slice transmission, ownership and integrity are verified through weighted encoding, with the verification basis derived from the interleaved weighting information in the lightweight encoding index.

8. The method according to claim 6, characterized in that, The frame-level slicing and reconstruction of interstellar voice and video information follows a scenario-based strategy: in tourism scenarios, the core video footage and voice guidance are restored first; in mining scenarios, the equipment status and control command feedback are restored first; in scientific research scenarios, the key frames of observation video and analysis voice are restored first; and in logistics scenarios, the material location and status broadcast are restored first. The scene-based reconstruction and slicing recombination strategy for photon expansion is matched, prioritizing the restoration of light and shadow and dynamic features in tourism scenes, and prioritizing the restoration of structural and data features in mining and scientific research scenes, with output parameters dynamically adapted according to the scene.

9. A digital personality replication and carbon-silicon symbiosis terminal device, characterized in that, The system, equipped with the core module of any one of claims 1 to 5, includes at least one of smart glasses, holographic projection equipment, non-invasive brain-computer interface, implantable chip, multi-scenario silicon-based robot, military terminal, and aerospace equipment. Each device is equipped with a three-core hardware architecture consisting of a personality chip and dual storage media, following a computational core and categorized storage logic: the personality chip has a built-in gene-driven self-evolution mechanism, providing local computation, encoding / decoding, and self-evolution capabilities; the dual storage media are categorized and deployed according to the entity's behavior (read-only storage) and real-time acquisition (rolling over) storage. The device supports gradient compression ratio adaptation, possesses autonomous operation capabilities, can operate independently without a network for N43 days, and supports autonomous fault repair and incremental feature self-learning. The device can achieve real-time interstellar voice and video interaction and three-dimensional spatial feature restoration; the perception latency is adapted according to scenario gradients: W50ms for lunar and Martian scenarios, W10ms for Mercury scenarios, and W0.01ms for Europa scenarios; the hardware environment tolerance parameters are adapted according to application scenarios to meet the operational requirements of extreme environments.

10. The system according to claim 1 or the method according to claim 6, characterized in that, The system comprises a minimum complete set of technologies, consisting of "three core hardware architectures, lightweight coding indexes, gradient compression ratio algorithms, photon expansion mechanisms, light-speed delay cache synchronization, and gene-driven self-evolution mechanisms," none of which can be omitted. Any technical solution that imitates any core feature of this set of technologies, regardless of whether it adds, modifies, or downgrades hardware parameters, or makes any adjustments to terminal form, deployment scenarios, or technical details, constitutes substantial equivalent infringement. Both the Earth-based main base station and the base stations on each planet are equipped with the three core hardware architectures. The Earth-based main base station is configured with an N2000PFL0PS computing power cluster and dual 20PB redundant storage arrays, serving as the central hub for scheduling across the entire solar system. Each planetary base station is configured with hardware according to the corresponding compression ratio gradient. Data from distant planets is relayed through neighboring base stations. When a base station fails, a neighboring base station automatically takes over. Each base station synchronizes scheduling logs and equipment status to the Earth-based main base station every hour. During scheduling, priority is given to ensuring the transmission efficiency of high-priority signals, with the priority order being: life safety signals > operation instruction signals > data acquisition signals > backup data signals. The scheduling data uses a lightweight encoded index as its sole carrier, and relies on a three-core hardware architecture to achieve secure storage and efficient computation.

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