88 results about "Ground system" patented technology

The invention relates to the technical field of satellite attitude control, in particular to a satellite-borne laser semi-autonomous pointing control method, electronic equipment and a storage medium. The method is completed by cooperation of a ground system and an on-satellite system, the ground system calculates a top target passing moment T * in advance, generates a unified laser pointing control instruction and injects the instruction into a satellite; and the satellite-borne system receives and analyzes the instruction, obtains parameters such as T * and beam selection, and then autonomously controls a specified load for work preparation. And the satellite-borne system autonomously calculates the optimal moment T1 and the target attitude when passing through the calibration field through high-precision orbit extrapolation based on the latest navigation data, finally autonomously executes attitude maneuver and laser pointing tasks, and autonomously returns after the tasks are completed. Instructions in a uniform format are generated and injected from the ground, ground operation is greatly simplified, efficient cooperation of ground decision triggering and on-satellite autonomous execution is achieved, pointing errors caused by orbit extrapolation are greatly reduced, the pointing precision and the task success rate are improved, and universality is good.

The invention relates to the technical field of unmanned aerial vehicle radio detection, in particular to an unmanned aerial vehicle detection and judgment method based on cooperation of an air-ground system and radio detection, and the method comprises the steps: finding a suspected target through scanning of a multi-frequency-band radar, triggering an infrared thermal imager carried by an aerial unmanned aerial vehicle to approach an ultra-wide-frequency-band spectrum sensor for verification; accurate positioning is realized by combining ground photoelectric equipment multi-view triangulation positioning and a signal arrival time difference algorithm, a command and control center calculates threat levels through a multi-source data fusion engine, and navigation decoy of dynamically adjusting intensity is adopted for targets smaller than or equal to two levels. Hard killing of ground laser locking rotor center and air electromagnetic pulse synchronous coverage is executed on a target of more than or equal to three levels, the equipment state is synchronized in real time through an optical fiber link, high-energy-consumption equipment is intelligently closed after threat is relieved, a platform starting strategy is optimized, a detection closed loop of'three-dimensional perception-graded treatment-intelligent energy saving 'is constructed, and the intelligent energy saving effect is achieved. And an efficient and accurate low-altitude safety protection scheme is provided for a sensitive area.

The present invention discloses a ground operation and application integrated system for high-resolution remote sensing satellites. Guided by the support for the operation and application of high-resolution satellites, an integrated space-ground system integrating the design, testing, operation control and application of high-resolution remote sensing satellites is first established to achieve the interconnection and interoperability of high-resolution remote sensing satellite design simulation, comprehensive test verification, on-orbit operation management, and comprehensive application of business data. Then, driven by requirements, an automated task planning and scheduling strategy is constructed to achieve task conflict resolution and optimal planning. Secondly, a training set of typical targets is established, and target intelligent interpretation is realized based on machine learning, effectively improving the timeliness and accuracy of target recognition and confirmation. Finally, data such as meteorology, hydrology, surveying and mapping, and basic maps are introduced to construct target information combined with the three-dimensional environment, and the overall situation awareness of the scene and the target is realized after visualization.

The invention discloses a seabed shallow casing section thermal insulation structure for polar region supercritical carbon dioxide drilling, which comprises a casing, a thermal insulation coating, a protective coating, an annular cement slurry layer, an electric heating pipe, a sensor module, a wireless conductive module, a ground system and a seabed wireless transmission module, and is characterized in that the electric heating pipe is fixed on the outer wall of the casing through a hoop; the outer wall of the casing pipe is sequentially coated with a heat preservation coating, a protective coating and an annular cement paste layer from inside to outside, the wireless conductive module is integrated at the end of the casing pipe, and the ground system comprises a ground data acquisition system and a ground control center. The sea surface platform is provided with a ground data acquisition system and a ground control center which are connected with the seabed wireless transmission module through an umbilical cable, and temperature and pressure data acquired by the sensor module are uploaded to the ground control center. According to the invention, the problems of rapid heat loss, annular air channeling, casing mechanical property degradation, poor drilling fluid fluidity and the like of the seabed shallow casing section in the polar region extreme low-temperature environment are solved.

Methods, systems, and apparatus, including computer programs encoded on computer-storage media, for ground system techniques to support flexible reconfigurable satellite payload operation. In some implementations, a satellite communication network is managed to operate in a first configuration. The satellite communication network includes a satellite having a payload that enables dynamic reconfiguration of carriers within a beam. A reconfiguration event is detected, and in response, a second configuration is determined for the satellite communication network. The second configuration differs from the first configuration in at least one of a set of carriers used for the beams or an assignment of the carriers to gateways. The satellite network is managed to operate in the second configuration, including at least one of (i) changing to a second set of carriers for the beams of the satellite or (ii) changing to a second assignment of the carriers to the gateways.

The application discloses a data transmission method, system and equipment of an array receiving acoustic logging instrument, a panoramic acoustic imaging logging instrument adopts a method of underground large data storage and two-way data transmission with a ground system, function implementation is realized by combination of a data acquisition module, a main control module and a data storage module, demodulation of a command sent by the ground system is realized, six acoustic transducer transmission modes are realized, a large amount of data of 96 full wave trains received in each mode is transmitted and stored underground, instrument state data and part of logging data are sent to the ground system, underground large data storage and two-way data transmission with the ground system are realized, and the problem that data cannot be transmitted to the ground system in real time and stored in real time due to limitation of a long cable data transmission rate in actual application is solved.

The invention relates to a remote sensing satellite observation result judgment method oriented to multi-factor influence. The method comprises the following steps: satellite load classification and task acquisition; satellite detection decision: according to the satellite task parameters, the observed target state, the environmental influence factors and the decision probability table, probability quantitative decision is carried out, and a satellite detection decision result is generated; data downloading judgment is carried out; target processing identification judgment: generating a target processing identification judgment result according to satellite and ground system parameters, a data transmission error rate, observed target characteristics and the like; and observation result generation: generating a target observation result according to a target identification processing result in combination with processing identification time, satellite load positioning errors and the like, and sending the target observation result to an information receiver. According to the method, the influence of different load types and different factors on target detection can be comprehensively considered, and meanwhile, a probability thinking method in the game theory is used for reference, so that rapid judgment of observation of the target by remote sensing satellites of different load types in a simulation deduction process is realized.

The invention relates to the technical field of intelligent control, in particular to a static meteorological satellite dynamic task intelligent control method, which enables a static meteorological satellite ground system to realize automatic execution and quick response of a dynamic task through an intelligent control algorithm and flow when facing the dynamic task. And the requirements in the aspects of emergency response requirements, meteorological service guarantee, satellite safety management and the like are effectively met. According to the intelligent control strategy, the intelligent level and the operation efficiency of the system are improved, and more accurate and efficient services are provided for meteorological observation and satellite operation; meanwhile, diversified meteorological service requirements can be better met, the efficiency and reliability of meteorological observation and disaster early warning are improved, and the risk of manual operation is reduced.

The present invention discloses a ground-to-rocket IO signal transmission system and method based on optical fiber medium. The on-rocket system terminal device includes a signal redundancy processing module and three signal conversion and processing modules; the ground system terminal is symmetrically equipped with three signal conversion and processing modules and an IO signal redundancy processing module; the on-rocket system terminal and the ground system terminal perform signal transmission through three optical fiber cables. The present invention realizes the fiberization of the ground-to-rocket IO signal transmission, and at the same time effectively improves the reliability and real-time performance of signal transmission by using a unique three-channel hardware redundancy processing method. Through the conversion and processing of the ground-to-rocket IO signal, the free configuration of the number of IO interfaces is realized, and the number of connector cores is effectively reduced; by adopting optical fiber medium transmission, the light weight of the cable is realized, and the electromagnetic compatibility performance of the cable is significantly enhanced; through the modular design concept, the convenient scheme configuration and upgrade and transformation are realized.

There is provided an artificial satellite and a ground system enabling to efficiently hold data in the artificial satellite. The artificial satellite includes an image processing unit that executes feature amount generation processing of generating a feature amount of a captured satellite image, a storage unit that holds feature amount data obtained as a result of the feature amount generation processing, and a communication unit that transmits the feature amount data to a ground station when communication with the ground station becomes possible. The ground system includes an image processing unit configured to generate complemented data by using complementing data and feature amount data that indicates a feature amount of a satellite image acquired from an artificial satellite and obtained by capturing an image of a ground by the artificial satellite.

This invention relates to the field of remote sensing satellite orbit control technology, and discloses a satellite autonomous pipeline control method based on differential interferometric SAR imaging missions. The method includes: acquiring initial satellite orbit parameters; employing a multi-objective optimization algorithm for orbit optimization under a high-order gravity field; sampling and constructing a reference orbit point set; calculating orbit control deviations based on the actual orbit and the reference orbit; generating orbit control triggering rules and avoidance strategies through ground system simulation; executing orbit control strategy generation and control onboard system; and evaluating orbit control effectiveness and the evolution trend of orbit control deviations through the ground system. Existing technologies mainly rely on ground command injection, making it difficult for satellites to achieve efficient autonomous orbit control when performing heavy-orbit differential interferometric SAR imaging missions, and hindering the decoupling of orbit control and imaging tasks. This invention improves the efficiency and autonomy of orbit control, the execution efficiency of imaging missions, and the safety of on-orbit operation by constructing a closed-loop control system encompassing satellite-ground collaboration, strategy formulation, command execution, and effect evaluation.

To achieve information on a mission device for executing mission other than communication via annular communication network in real time at low cost.SOLUTION: A hybrid constellation 20B formed in a Low Earth Orbit includes a communication constellation in which a plurality of satellites having a communication device communicating with precedent and following satellites in a travel direction on the same orbital plane form annular communication network 702, and a mission satellite 30b which has a communication device communicating with the precedent and following satellites, and a mission device for executing various missions. The mission satellite 30b flies between the plurality of satellites forming the communication constellation, the hybrid constellation 20b is formed by reconstruction of the annular communication network 702 using a plurality of satellites forming the communication constellation forming the annular communication network 702 and the mission satellite 30b.SELECTED DRAWING: Figure 17

The present invention discloses a method and system for high-precision positioning of on-orbit targets based on space-ground collaboration, belonging to the technical field of space remote sensing monitoring. It includes real-time on-orbit target recognition, imaging ray calculation, camera calibration, and ground coordinate calculation. The remote sensing image data and attitude auxiliary information collected on the satellite complete the recognition and extraction of the target through target recognition respectively. The imaging ray calculation completes the calculation of the imaging ray vector, and then is transmitted to the satellite ground processing system through the space-ground transmission link. The precise coordinates of the target are calculated according to the digital elevation, and then compared with the control point library to determine whether this target is a control point with known three-dimensional coordinates. If it is a control point, it is input into the camera calibration module of the on-orbit system to calculate the camera calibration parameters. This method can make full use of the respective advantages of the on-orbit system and the ground system, optimize the real-time on-orbit target recognition process, and improve the acquisition efficiency and real-time performance of on-orbit targets.

The invention belongs to the technical field of near-infrared signals, and particularly relates to a laser target spot instrument testing device and method. The laser target spot instrument testing device comprises a target spot instrument system, an unmanned aerial vehicle system and a ground system, and a strong light processing unit which is used for carrying out attenuation processing on incident strong light and converting the incident strong light into an analog signal; the data acquisition unit is used for receiving and conditioning the analog signal and converting the analog signal into a digital signal; the data control unit is used for receiving and optimizing the digital signal; the thermal management unit is used for monitoring, pre-judging and intelligently and dynamically regulating and controlling the temperature of the target spot instrument system in real time; the unmanned aerial vehicle system is used for controlling the flight of the unmanned aerial vehicle and transmitting the attitude information of the unmanned aerial vehicle to the ground system in real time; the ground system is used for receiving the attitude information of the unmanned aerial vehicle and the optimized digital signal, processing the optimized digital signal and displaying signal data; meanwhile, a flight adjustment instruction is sent to the unmanned aerial vehicle system, and a data acquisition unit adjustment instruction is sent to the target spot instrument system.

This application belongs to the field of unmanned aerial vehicle (UAV) and data communication technology, and specifically relates to a UAV data transmission verification method based on the MD5 algorithm. The method involves extracting flight path data in a pre-defined order, calculating the MD5 "fingerprint" value of the flight path data, and transmitting the MD5 "fingerprint" value to the ground. The ground system calculates the MD5 "fingerprint" value of the ground flight path data in the same pre-defined order and compares it with the MD5 "fingerprint" value transmitted from the UAV. If the MD5 "fingerprint" values ​​match, the flight path stored by the UAV is correct and usable; if the MD5 "fingerprint" values ​​do not match, it indicates that the flight path stored by the UAV is incorrect and needs to be reloaded. The data is protected from interception and is not easily exposed: using the MD5 algorithm to verify the accuracy of flight path data does not require transmitting all flight path data, thus eliminating the risk of data interception. Furthermore, only one frame of data needs to be transmitted back, which significantly reduces the risk of exposure, especially for stealth aircraft.

This invention proposes a method for autonomous collaborative satellite selection for high-orbit tracking and guidance of moving targets, enabling the identification of low-Earth orbit (LEO) satellites. A high-orbit remote sensing satellite detects and tracks a moving target, autonomously detecting the target through onboard information processing and calculating its current position, velocity, direction, shortest side length, and corresponding time as guidance information for collaborative observation. The ground system pre-injects collaborative observation requirements and candidate LEO satellite information onto the high-orbit remote sensing satellite. Based on this candidate LEO satellite information, the high-orbit remote sensing satellite's own on-orbit operation status, and imaging performance parameters, it calculates and assesses the imaging and target recognition capabilities of all candidate LEO satellites when observing the moving target. The high-orbit remote sensing satellite then selects candidate satellites whose estimated imaging and target recognition capabilities meet the collaborative observation requirements, serving as the first round of candidate satellites for collaborative observation.

The invention discloses an anti-ground-touching method and an anti-ground-touching system for a working column, and relates to the technical field of working vehicle construction safety monitoring, the anti-ground-touching method for the working column comprises the steps that real-time monitoring data of a pressure sensor and a strain sensor are acquired, the pressure sensor and the strain sensor are arranged at the connecting position of the working column and a fixing frame, and the pressure sensor and the strain sensor are connected; the real-time monitoring data is used for representing the state of the workbar; comparing the real-time monitoring data with the initial data of the pressure sensor and the strain sensor; if the real-time monitoring data is greater than the initial data, representing that the workbar is in a bearing state, and controlling and keeping the operation state of the workbar; and if the real-time monitoring data is smaller than the initial data, representing that the workbar is in a state of touching the ground or encountering an obstacle, and controlling the operation state of the workbar to perform safety intervention. According to the working bar grounding prevention method, the working platform can be reliably prevented from grounding, the working safety is ensured, and the maintenance cost is reduced.

The invention provides a ground wire detection device and a ground wire detection method. The ground wire detection device comprises a power supply module, a measuring resistor, a regression wire and a control module, the positive electrode of the power module is electrically connected with the first end of the grounding wire and a first grounding system through the measuring resistor, the negative electrode of the power module is electrically connected with the first end of the return wire, and the second end of the return wire is electrically connected with the second end of the grounding wire and a second grounding system. The control module is used for detecting the line voltage between the first end of the grounding line and the first end of the regression line, and according to the line voltage, the power supply voltage between the positive electrode and the negative electrode of the power supply module, the measurement resistance value of the measurement resistor, the regression line resistance value of the regression line and the equivalent resistance value range between the first grounding system and the second grounding system. And obtaining the grounding wire resistance value range of the grounding wire. Current detection does not need to be carried out on the ground wire, and the reliability of the whole impedance detection is improved.

The application relates to a kind of air-ground transient electromagnetic self-adapting air collection methods, comprising: through transient electromagnetic receiver pre-collection time series data;The measured time series data is analyzed, and the adjacent two positive and negative extreme values are selected in the measured secondary field data, the time interval of the two places is divided by 2, and the time base parameter of the transmission waveform is obtained;Platform time period is identified in the measured signal, and the Ramp parameter in the transmission waveform corresponding to the time is obtained;The measured time series data is correlated with the standard secondary field periodic signal;Transient electromagnetic receiver starts synchronization according to the time base integer multiple of the starting time of transmission waveform, collects according to logarithmic interval window, superimposes data, and completes the data collection of one point;The receiver continues to collect on the flight platform according to the set route until the completion of all survey lines.The application can be compatible with multiple transmission systems, realize automatic analysis of transmission parameters under the condition of any ground system transmission, find the synchronous starting position and complete data collection.

The invention provides a ground system suitable for a whole-process automatic test of a moonlet measurement and control subsystem, and the system comprises a measurement and control signal processing module which comprises an upper frequency conversion sub-module, an intermediate frequency modulation sub-module, an intermediate frequency demodulation sub-module, a lower frequency conversion sub-module, and a local oscillator sub-module; the channel adjusting module comprises an uplink programmable attenuator, a downlink programmable attenuator, a power divider, a combiner, a circulator, an uplink switch, a downlink switch and a coupling detector; the centralized management and control module is used for issuing working parameters of the measurement and control signal processing module and the channel adjustment module, collecting working states and splicing whole-process working nodes; the centralized management and control module comprises an upper computer sub-module and a centralized agent sub-module, the upper computer sub-module is used for configuring and displaying working parameters of the measurement and control signal processing module, establishing a measurement channel for a measurement and control system, resolving and counting data, and the centralized agent sub-module is used for managing each sub-module in the channel adjustment module.

The invention discloses a flight waypoint monitoring method, system, equipment and medium, and the method comprises the steps: firstly obtaining the current information and planned waypoint data of an aircraft, then calculating a front waypoint and a rear waypoint of the current position of the aircraft according to the current information and the planned waypoint data, and then calculating the front waypoint and the rear waypoint of the current position of the aircraft; the method comprises the following steps: acquiring a front waypoint and a rear waypoint of an airplane, respectively recording a distance change trend between the current position of the airplane and the front waypoint as well as the rear waypoint at continuous time intervals, judging the moment when the airplane flies over the rear waypoint according to the distance change trend, and when the airplane flies over the rear waypoint, recording waypoint data, and finally, according to the deviation value of the planned waypoint data and the flyover waypoint data, carrying out real-time optimization on the flight plan of the aircraft, and after the flight is finished, returning related data to a ground system so as to assist in improving the accuracy of making a future flight plan. According to the invention, the timeliness, accuracy and efficiency of actual waypoint data recording in flight can be improved, and the flight safety is further guaranteed.

This invention provides a comprehensive evaluation method for the mid-frequency performance of a filter field grounding system, belonging to the field of power grid equipment technology. The invention extracts the resonant frequency distribution by inputting a wideband impedance spectrum into an artificial intelligence frequency domain response identification model based on a coarse spatiotemporal attention mechanism. It then dynamically adjusts the spatial receptive field parameters according to the resonant frequency offset function. A three-dimensional electromagnetic field simulation model is established based on soil frequency domain parameters, and the ground potential and current density distribution are calculated using the radial basis function collocation method and the fast multipole algorithm. The entropy value of current distribution uniformity and the Gini coefficient are calculated to identify current concentration areas and assess local overheating risk. Finally, the analytic hierarchy process (AHP) is used to dynamically weight and comprehensively score indicators such as impedance peak value, resonant frequency, ground potential gradient, current uniformity, and overheating risk. This invention solves the technical problem of inaccurate performance evaluation of filter field grounding systems under mid-frequency impulse conditions.

The application discloses a low-orbit satellite communication system time difference estimation method based on burst time slot capture. In the low-orbit satellite communication system, the satellite and the ground are synchronized with the same time reference, but due to the influence of the low-orbit satellite-ground system time precision, the synchronization is not complete, and even after compensation, there is an unknown residual time difference. Therefore, the burst signal sent by the ground terminal in the low-orbit satellite communication system will be ahead of or lag behind the time slot, the demodulator on the low-orbit satellite accurately calculates the time difference value of the burst signal ahead of or lagging behind the current time slot by using the mathematical relationship between the time counting of each time slot and the capture of the burst signal, takes the time difference value as the time difference estimation value, packs the time difference value as part of the demodulation information, and uploads the time difference value to the upper layer of the satellite for distribution. On the basis of the pre-calculated time difference, the ground terminal repeatedly compensates and corrects the time difference estimation value distributed by the satellite, and the accuracy of the satellite-ground closed-loop time difference adjustment is improved.

This invention discloses a millimeter-level monitoring method and system for geological deformation in mining areas based on an integrated space-air-ground system, relating to the field of geological monitoring technology. The method includes: acquiring time-series synthetic aperture radar (SAR) images, GNSS observation data, and subsurface microseismic data; inverting the physical property parameters of the surface cover medium based on GNSS observation data, calculating the medium phase delay, and compensating for the original interferometric encapsulation phase to obtain the true geometric encapsulation phase; performing spatial clustering based on subsurface microseismic data to extract fault rupture surfaces and generate discontinuous masks, which are then superimposed onto the true geometric encapsulation phase to block cross-fault phase unwrapping paths, dividing the mining area into multiple topologically isolated blocks and performing independent phase unwrapping on each; acquiring the absolute deformation projection values ​​of GNSS stations within each block, combining the unwrapped phase to calculate the reference intercept, and reconstructing the continuous absolute deformation field of the mining area; this invention achieves high-precision monitoring of mining area deformation through medium phase compensation and fault topological constraints.

The application discloses a kind of high-low orbit satellite guidance observation-oriented mission planning methods, belong to the field of spaceflight ground system operation and control.The method is directed to high-orbit satellite guides low-orbit satellite observation scene and low-orbit satellite guides high-orbit satellite observation scene, using the chainable period of two satellites of high-low orbit, the observable period of low-orbit satellite to observation target and relevant parameters, mission planning is carried out, the observation period of high-orbit satellite is determined, and the satellite observation sequence combination of high-low orbit satellite guidance observation task is generated.The application can solve the planning problem of high-low orbit satellite mutual guidance observation, can generate the satellite observation sequence combination of actually usable high-low orbit satellite guidance observation task, improve the overall use efficiency of satellite.

The utility model provides a positioning device for directional perforation based on distributed optical fibers. The positioning device comprises a perforation gun rotation control device, an audio signal generation device, a depth correction device, a perforation gun string and a pumping ring which are arranged in a sleeve, the perforating gun rotation control device and the audio signal generation device are connected with the ground system through cables respectively; the perforating gun rotation control device comprises a first fixed part and a first rotating part; the lower end of a first rotating part of the perforating gun rotating control device is connected with a perforating gun string; the perforating gun string is connected with a pumping ring; the audio signal generating device comprises a second fixed part and a second rotating part, the second rotating part synchronously rotates along with the first rotating part, and a sound wave transducer is arranged in the second rotating part. According to the invention, the positioning control of the tripping-in tool is realized, so that the perforating gun is adjusted to the orientation meeting the design requirement. The device is simple in structure and easy to implement, and the adjustment of the perforating gun can be accurately mastered.

A ground system for satellite-borne synthetic aperture radar external correction comprises an antenna housing which is integrally provided with a receiving antenna and a transmitting antenna; the first azimuth angle adjusting device is used for adjusting the azimuth angle of the antenna shell; the second height adjusting device is used for controlling the height of the antenna shell; a satellite orientation control unit that receives a position of a satellite from the satellite or a satellite regulation server and controls the first azimuth angle adjustment device and the second height adjustment device such that the receiver and the transmitter point to the received position of the satellite; the receiving antenna is used for receiving a synthetic aperture radar signal of a satellite; the amplifier is used for amplifying the satellite radar signal of the receiving antenna; and a transmitting antenna that transmits the satellite radar signal amplified by the amplifier toward a satellite.

A compact system and method for two-way communication via digital radio modes, such as FT4 and FT8, are disclosed. The system includes a multiband transceiver, protol definition files, an audio signal generator, a digital signal processor, an monopole antenna system, a ground system with a ground plane, solar power supply, and a computer interface with input and output capabilities. The system scans a predefined spectrum slice, detects digital mode signals, decodes them, and displays the results on a waterfall display. Users can input data by selecting icons or via a keyboard or microphone, with the latter employing speech-to-text conversion. A user-friendly interface allows message encoding and transmission by selecting specific options, ensuring efficient use of frequency bands licensed for amateur radio. The system is easily adaptable for use by other classes of radio operator.

This invention relates to the field of remote sensing data processing technology, specifically to a satellite-ground integrated distributed processing method for remote sensing constellation data, comprising the following steps: S1: acquiring raw remote sensing images in orbit; S2: performing data preprocessing on the raw remote sensing data, including radiometric calibration, sensor correction, and geometric coarse correction; S3: performing rapid region segmentation and ground feature classification and initial screening; S4: making task coordination and distribution decisions based on the confidence level C and type Type of each initially screened target; S5: data encapsulation and downlink, encapsulating the data to be transmitted back to the ground; S6: ground system reception, receiving the data packets transmitted from satellite; S7: the ground system distributes the data to the corresponding dedicated processing algorithm for final image interpretation and processing based on the data information. This invention creatively designs a "coarse screening-distribution" satellite-ground collaborative processing flow and a multi-level processing architecture of "main satellite distribution-constellation system-ground fine interpretation".