A phase shift and time delay calculation method and system for a near field communication and sensing integrated system
By calculating the phase shift of each phase shifter in the system and the delay range of the delay module, the three-dimensional beamformer design is optimized, which solves the problem of performance degradation of the communication and perception integrated system caused by the beam squint effect, and achieves a balance between high perception coverage range and high communication rate.
Patent Information
- Application Number
- CN202411467867.8
- Authority / Receiving Office
- CN · China
- Patent Type
- Patents(China)
- Current Assignee / Owner
- Filing Date
- 2024-10-21
- Publication Date
- 2025-10-24
- Estimated Expiration
- 2044-10-21
AI Technical Summary
Existing technologies fail to effectively design an integrated near-field communication perception system with beam squint effect, resulting in a decline in the performance of the communication and perception processes, and unable to simultaneously meet the requirements of high perception coverage and high communication user rate.
By calculating the phase shift of each phase shifter in the system and the delay range of each delay module, combined with the preset perception coverage and resolution, the design of the three-dimensional beamformer is optimized to achieve controllable beam squint and maximize the achievable rate of communication users.
While ensuring sufficient sensing coverage and resolution, it significantly improves the reachability rate for communication users and enhances the overall performance of the near-field sensing integrated system.
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Figure CN119342516B_ABST
Abstract
Description
TECHNICAL FIELD
[0001] The present application relates to the technical field of wireless communication, in particular to a phase shift and time delay calculation method and system for a near-field communication and sensing integrated system. BACKGROUND
[0002] With the development of the 6th generation mobile communication system (6G), communication and sensing integrated technology has attracted great attention, providing reliable low-latency links, higher communication transmission rates, and high-resolution and robust sensing capabilities for emerging 6G applications. In a communication and sensing integrated system, communication signals can be used for positioning services of sensing targets, greatly reducing the related overhead of dedicated radar signals.
[0003] In addition, to meet the higher performance requirements of 6G for communication and sensing, super large-scale MIMO technology and high-frequency communication technology (such as millimeter wave) need to be introduced. On the one hand, super large-scale MIMO technology significantly improves system spectral efficiency and spatial resolution by deploying super large antenna arrays, and also leads to a fundamental change in channel modeling of electromagnetic wave propagation, i.e., from far-field channel modeling to near-field channel modeling; on the other hand, the increasing antenna array size and transmission bandwidth lead to beam squint effect, which significantly reduces the performance of traditional communication and sensing integrated systems. Specifically, the beam squint effect causes the analog beamforming direction to change with frequency, resulting in severe energy leakage. At the same time, the sensing process benefits from the beam squint channel containing more potential information, and through the beams focused on different positions generated at different frequencies, the sensing process has the potential to collect more comprehensive information from the channel environment. However, existing technologies often only focus on eliminating the beam squint effect to improve system communication performance or using the beam squint effect for target estimation, and do not design for near-field communication and sensing integrated systems considering the beam squint effect to simultaneously perform communication and sensing processes. SUMMARY
[0004] The purpose of the present application is to overcome the deficiencies in the prior art and provide a phase shift and time delay calculation method and system for a near-field communication and sensing integrated system to simultaneously perform communication and sensing processes, maximizing the achievable rate of communication users while ensuring sufficient sensing coverage and sensing resolution.
[0005] To achieve the above purpose, the present application adopts the following technical solutions:
[0006] On the one hand, the present application provides a phase shift and time delay calculation method for a near-field communication and sensing integrated system, comprising:
[0007] Calculate the phase shift of each phase shifter in the system and the initial delay range of each delay module based on the preset system perception coverage, antenna spacing, system minimum frequency, system maximum frequency, and system bandwidth; wherein the preset system perception coverage includes a preset perception angle domain coverage and a preset perception distance domain coverage;
[0008] Calculating the final delay range of each delay module of the system according to a preset system perception resolution, a preset system perception coverage range, antenna spacing, a system minimum frequency, a system maximum frequency, and a system bandwidth; wherein the preset system perception resolution includes a preset perception angle domain resolution and a preset perception distance domain resolution;
[0009] Within the final delay range, obtain the delay of each delay module when the communication user's achievable rate is maximized.
[0010] Optionally, the preset system perception coverage is expressed as:
[0011] ;
[0012] Where, Indicates the distance within the preset system perception coverage range; Indicates the physical azimuth within the preset system perception coverage range; Indicates the physical pitch angle within the preset system perception coverage range; and Respectively represent the minimum distance and maximum distance within the preset system perception coverage range; and Respectively represent the minimum physical azimuth and maximum physical azimuth within the preset system perception coverage range; and They respectively represent the minimum physical pitch angle and the maximum physical pitch angle within the preset system perception coverage range.
[0013] Optionally, the phase shift of each phase shifter in the system is expressed as:
[0014] ;
[0015] ;
[0016] ;
[0017] Where, Indicates the Phase shift of a phase shifter; Indicates the lowest frequency of the system; represents the speed of light; and Respectively represent row index and column index of a phase shifter; denotes the antenna spacing; denotes the minimum spatial azimuth angle and the minimum spatial elevation angle in the preset system awareness coverage range, respectively; denotes the minimum spatial azimuth angle and the minimum spatial elevation angle in the preset system awareness coverage range, respectively; denotes the minimum distance in the preset system awareness coverage range; denotes the minimum physical azimuth angle in the preset system awareness coverage range; denotes the minimum physical elevation angle and the maximum physical elevation angle in the preset system awareness coverage range, respectively; denotes the minimum physical elevation angle and the maximum physical elevation angle in the preset system awareness coverage range, respectively.
[0018] Optionally, the initial delay range of each delay module of the system is represented as:
[0019] ;
[0020] wherein,
[0021] ;
[0022] ;
[0023] wherein, denotes the initial delay range of the first delay module in the first layer; denotes the initial delay range of the first delay module in the first layer; denotes the initial delay range of the first delay module in the first layer; denotes the initial delay range of the first delay module in the first layer; denotes the minimum delay that can be achieved by the first delay module in the first layer and the second delay module in the second layer, respectively; denotes the minimum delay that can be achieved by the first delay module in the first layer and the second delay module in the second layer, respectively; denotes the highest frequency of the system; denotes the antenna spacing; denotes the minimum spatial azimuth angle and the maximum spatial azimuth angle in the preset system awareness coverage range, respectively; denotes the lowest frequency of the system; denotes the bandwidth of the system; denotes the minimum spatial elevation angle and the maximum spatial elevation angle in the preset system awareness coverage range, respectively; denotes the lowest frequency of the system; denotes the bandwidth of the system; denotes the minimum spatial elevation angle and the maximum spatial elevation angle in the preset system awareness coverage range, respectively; denotes the minimum distance and the maximum distance in the preset system awareness coverage range, respectively. Optionally, the preset system awareness angle domain resolution is represented as:
[0024]
[0025] ;
[0026] Where, Indicates the total number of subcarriers; Indicates the subcarrier index; and Respectively represent Subcarrier and The physical azimuth of the beam corresponding to the subcarrier; and Respectively represent Subcarrier and The physical elevation angle of the beam corresponding to the subcarrier; Indicates a 3 dB beamwidth.
[0027] Optionally, the preset system perception distance domain resolution is expressed as:
[0028] ;
[0029] Where, Indicates the total number of subcarriers; Indicates the subcarrier index; and Respectively represent Subcarrier and The distance of the beam corresponding to the subcarrier; Indicates 3 dB beam depth; represents the array aperture; Indicates wavelength; Indicates the number of base station antennas; Indicates the antenna spacing.
[0030] Optionally, the final delay range of each delay module in the system is expressed as:
[0031] ;
[0032] in,
[0033] ;
[0034] ;
[0035] ;
[0036] ;
[0037] Where, Indicates the first layer The final delay range of each delay module; Indicates the second layer The final delay range of each delay module; and Represents the first layer The delay module and the second layer The maximum delay that can be achieved by a delay module; Indicates the highest frequency of the system; Indicates the antenna spacing; and They represent the minimum spatial orientation angle within the preset system perception coverage range and the maximum spatial orientation angle under the preset system perception resolution, respectively; and They represent the minimum distance within the preset system perception coverage range and the maximum distance under the preset system perception resolution respectively; Indicates the lowest frequency of the system; Indicates the system bandwidth; and They respectively represent the minimum spatial pitch angle within the preset system perception coverage range and the maximum spatial pitch angle at the preset system perception resolution; and They respectively represent the maximum physical azimuth and maximum physical elevation angles under the preset system perception resolution.
[0038] Optionally, the delay of each delay module when the communication user achievable rate is maximized is expressed as:
[0039] ;
[0040] ;
[0041] Where, Indicates the first layer under the maximum achievable rate of communication users The delay of each delay module; Indicates the second layer under the maximum achievable rate of communication users The delay of each delay module; Indicates the highest frequency of the system; Indicates the antenna spacing; and Respectively represent the minimum spatial orientation angle and the maximum spatial orientation angle within the preset system perception coverage range; Indicates the lowest frequency of the system; Indicates the system bandwidth; and They represent the minimum and maximum spatial pitch angles within the preset system perception coverage range respectively; and They represent the minimum and maximum distances within the preset system perception coverage range respectively.
[0042] In a second aspect, the present application provides a computer system, comprising:
[0043] a memory for storing computer instructions;
[0044] a processor for executing the computer instructions to implement the steps of the phase shift and time delay calculation method for the near field communication and sensing integrated system according to the first aspect.
[0045] In a third aspect, the present application provides a computer readable storage medium having stored thereon a computer program, which, when executed by a processor, implements the steps of the phase shift and time delay calculation method for the near field communication and sensing integrated system according to the first aspect.
[0046] Advantages
[0047] Compared with the prior art, the present application has the following advantages:
[0048] The near field communication and sensing integrated system according to the present application considers the sensing resolution, which considers both the sensing angle resolution and the sensing distance resolution, and realizes the communication and sensing processes, maximizes the reachable rate of the communication users under the condition of ensuring sufficient sensing coverage and sensing resolution, and has significant advancement and effectiveness. BRIEF DESCRIPTION OF DRAWINGS
[0049] Figure 1 Fig. 1 shows a flowchart of the phase shift and time delay calculation method for the near field communication and sensing integrated system according to the present application in an embodiment;
[0050] Figure 2 Fig. 2 shows a structural schematic diagram of the near field communication and sensing integrated system according to the present application in an embodiment;
[0051] Figure 3 Fig. 3 shows a simulation result schematic diagram of the phase shift and time delay calculation method for the near field communication and sensing integrated system according to the present application in an embodiment;
[0052] In the figure: 1 - dual-function base station; 2 - communication user; 3 - sensing target. DETAILED DESCRIPTION
[0053] The technical solutions of the present application will be described in detail below with reference to the accompanying drawings and specific embodiments. It should be understood that the embodiments of the present application and the specific features in the embodiments are detailed descriptions of the technical solutions of the present application, and are not limitations of the technical solutions of the present application. In the case of no conflict, the technical features in the embodiments of the present application and the embodiments can be combined with each other.
[0054] The term "and / or", only describes the association relation of the associated objects, which means that there can be three kinds of relations, for example, A and / or B, which can represent the three cases of A alone, A and B together, and B alone. In addition, the character " / " generally represents that the associated objects before and after are in an "or" relationship.
[0055] Embodiment 1
[0056] As shown in the figure, the embodiment introduces a phase shift and time delay calculation method for a near-field communication and sensing integrated system, which specifically includes the following steps: Figure 1
[0057] As shown in the figure, the structure schematic diagram of the near-field communication and sensing integrated system of the embodiment, including a dual-function base station 1, a communication user 2, and a sensing target 3. Figure 2
[0058] The dual-function base station 1 is used to transmit signals carrying communication information to provide downlink communication services for the communication user 2, and at the same time, based on the echo signal, to provide three-dimensional spatial positioning services for the sensing target 3. A time delay-phase shift architecture three-dimensional beamformer is used for transmitting beamforming design to realize controllable beam squint in an orthogonal frequency division multiplexing system, so as to maximize the communication performance of the system under the performance requirements of the sensing service.
[0059] The dual-function base station 1 is configured with a time delay-phase shift architecture three-dimensional beamformer, and two layers of time delayers and one layer of phase shifters are cascaded to constitute the three-dimensional beamformer.
[0060] The two layers of time delayers are respectively equipped with and a time delay module, and the phase shifter layer is equipped with a phase shifter. Each time delay module in the first layer of time delayers is connected to one end of each time delay module in the second layer of time delayers, each time delay module in the second layer of time delayers is connected to one end of each phase shifter in the phase shifter layer at the other end, and the other end of each phase shifter in the phase shifter layer is connected to the base station antenna one by one.
[0061] Therefore, the beamforming vector generated by the time delay-phase shift architecture three-dimensional beamformer can be represented as:
[0062] ;
[0063] Wherein, , represents the phase shift generated by the i-th phase shifter; and respectively represent the time delay generated by the i-th time delay module in the first layer of time delayers and the i-th time delay module in the second layer of time delayers. Therefore, the beamforming vector generated by the time delay-phase shift architecture three-dimensional beamformer can be represented as: a time delay generated by the time delay module; representing the first corresponding to the baseband frequency of the subcarrier.
[0064] Step one: set a preset system sensing coverage range, the preset sensing coverage range is a three-dimensional space coverage range, including a preset system sensing angle domain coverage range and a preset system sensing distance domain coverage range, wherein the preset system sensing angle domain coverage range includes a preset system sensing horizontal angle domain coverage range and a preset system sensing vertical angle domain coverage range, and the preset system sensing coverage range and the preset system sensing resolution are used as performance indicators of the near-field integrated sensing system.
[0065] Specifically, the three-dimensional beamformer transmits a beamforming design to realize a controllable beam squint in an orthogonal frequency division multiplexing system, so as to maximize the communication performance of the system while meeting the performance requirements of the sensing service.
[0066] To realize the controllable beam squint effect to complete the communication and sensing processes at the same time, the preset system sensing space, i.e., the preset system sensing coverage range, includes angle domain and distance domain information, and is represented as:
[0067] ;
[0068] In the formula, represents the distance within the preset system sensing coverage range; represents the physical azimuth angle within the preset system sensing coverage range; represents the physical pitch angle within the preset system sensing coverage range; and respectively represent the minimum distance and the maximum distance within the preset system sensing coverage range; and respectively represent the minimum physical azimuth angle and the maximum physical azimuth angle within the preset system sensing coverage range; and respectively represent the minimum physical pitch angle and the maximum physical pitch angle within the preset system sensing coverage range.
[0069] Step two: to meet the performance requirements of the preset system sensing coverage range, through analysis of the controllable beam squint effect, the configuration of the phase shifter in the three-dimensional beamformer should make the minimum angle and the minimum distance of the beam alignment sensing space on the 0th subcarrier of the orthogonal frequency division multiplexing system, i.e., , so that the phase shift of each phase shifter of the system can be obtained according to the near-field uniform spherical wave channel, and is represented as:
[0070] ;
[0071] in,
[0072] ;
[0073] ;
[0074] Where, Indicates the Phase shift of a phase shifter; Indicates the lowest frequency of the system; represents the speed of light; and Respectively represent The row and column indices of the phase shifters, , ; Indicates the antenna spacing; and They respectively represent the minimum spatial azimuth and minimum spatial elevation angle within the preset system perception coverage range.
[0075] Step 3: To meet the performance requirements of the preset system perception coverage, through the analysis of the squint effect of the steerable beam, the initial delay of the delay module in the first delay layer and the second delay layer should be such that the first delay module is The beam on the subcarrier is aligned with the maximum angle and maximum distance of the sensing space, that is, , so the initial delay range of each delay module in the system is expressed as:
[0076] ;
[0077] in, Indicates the first layer The initial delay range of each delay module; Indicates the second layer The initial delay range of each delay module; and Represents the first layer The delay module and the second layer The minimum delay that can be achieved by a delay module.
[0078] Analyzing the near-field uniform spherical wave channel, we obtain and As shown below:
[0079] ;
[0080] ;
[0081] Where, Indicates the highest frequency of the system; denotes the maximum spatial azimuth angle within the preset system perceived coverage range; denotes the system bandwidth; denotes the maximum spatial elevation angle within the preset system perceived coverage range.
[0082] Step four: setting a preset system perceived resolution, which includes a preset system perceived angle domain resolution and a preset system perceived distance domain resolution, wherein the preset system perceived angle domain resolution includes a preset system perceived horizontal angle domain resolution and a preset system perceived vertical angle domain resolution, and the achievable rate is taken as a performance indicator of the system communication service.
[0083] The preset system perceived angle domain resolution is described as follows: when any direction within the system perceived space can be covered by one perceived beam, it is considered that the system perceived angle domain resolution can be met, and to quantify this standard, it is required that the azimuth angle and elevation angle intervals between beams of adjacent subcarriers are both less than the 3-dB beam width of all directions in the system perceived space Therefore, the preset system perceived angle domain resolution performance requirement is expressed as follows:
[0084] ;
[0085] In the formula, denotes the total number of subcarriers; denotes the subcarrier index; and denote the physical azimuth angles of the beams corresponding to the th subcarrier and the th subcarrier, respectively; and denote the physical elevation angles of the beams corresponding to the th subcarrier and the th subcarrier, respectively; denotes the 3-dB beam width, which is inversely proportional to the number of base station antennas.
[0086] The preset system perceived distance domain resolution is described as follows: similar to the preset system perceived angle domain resolution, the beam depth is introduced to represent the system perceived resolution in the distance domain, and it is required that any position in the system perceived space is covered by the 3-dB beam depth of at least one beam, and to quantify this standard, it is required that the interval of focusing distances between beams of adjacent subcarriers is less than the 3-dB beam depth of all focusing distances in the system perceived space In addition, the system perceived space should meet the requirement of near-field beamforming in the distance domain, that is, Therefore, the preset system perception distance resolution performance requirement is expressed as follows:
[0087]
[0088] wherein, and respectively represent the distance of the beam corresponding to the first subcarrier and the first subcarrier; represents the 3 decibel beam depth; represents the array aperture; represents the wavelength; represents the number of base station antennas.
[0089] Step five: to meet the preset system perception resolution performance requirement, through the analysis of the controllable beam squint effect and the preset system perception resolution, the final time delay range of each time delay device module of the system is represented as:
[0090]
[0091] wherein, represents the final time delay range of the first time delay device module of the first layer; represents the final time delay range of the first time delay device module of the second layer; and respectively represent the maximum time delay that can be achieved by the first time delay device module of the first layer and the first time delay device module of the second layer.
[0092] For the analysis of the near-field uniform spherical wave channel, the and are as follows:
[0093]
[0094]
[0095] wherein,
[0096]
[0097]
[0098] wherein, represents the maximum spatial azimuth angle under the preset system perception resolution; represents the maximum distance under the preset system perception resolution; represents the maximum spatial elevation angle under the preset system perception resolution; and respectively represent the maximum physical azimuth angle and the maximum physical pitch angle under the preset system perception resolution, which are obtained by analyzing the performance requirements of the preset system perception angle resolution and the preset system perception distance resolution.
[0099] Step six: By analyzing the influence of phase shift and time delay on communication and perception performance, the time delay of each time delay module under the maximum communication user reachable rate is obtained within the final time delay range. Specifically, when and , the time delay that maximizes the communication performance of the system under the performance requirements of the perception service is obtained, and is expressed as:
[0100] ;
[0101] ;
[0102] In the formula, represents the time delay of the first time delay module in the first layer under the maximum communication user reachable rate; represents the time delay of the second time delay module in the second layer under the maximum communication user reachable rate. When or
[0103] , the preset system perception coverage range and the preset system perception resolution requirement are contradictory to each other, and at this time, the system is considered to be infeasible, and the system perception coverage range needs to be reduced or the system perception resolution requirement needs to be reduced to make the system feasible. In addition, for the time delays of the time delay modules in the first layer time delay and the second layer time delay and
[0104] , a delay should be introduced to ensure that the time delays generated by all time delay modules in the first layer time delay and the second layer time delay are positive, thereby completing the actual time delay circuit implementation. Embodiment 2
[0105] As shown in , this embodiment introduces a specific test design of a phase shift and time delay calculation method for a near-field sensing integrated system.
[0106] Figure 3 In this embodiment, the number of base station antennas in the communication and sensing integrated system is set to , the system carrier frequency is 60 GHz, the millimeter wave orthogonal frequency division multiplexing system bandwidth is 1 GHz, the subcarrier number is 128, the base station antenna spacing is half of the subcarrier wavelength, and the perception space
[0107] , using 3dB beam width and 3dB beam depth.
[0108] Figure 3 The two curves in the figure show the variation of the system communication rate with the transmitted signal-to-noise ratio, obtained using this embodiment and a traditional calculation method based on time-domain beam scanning. As can be seen, the solution proposed in this embodiment achieves a significant improvement in communication rate, validating the proposed phase shift and delay calculation method for a near-field synaesthesia integrated system. This method, based on near-field beam squint, simultaneously achieves communication and perception, maximizing the achievable rate for communication users while ensuring sufficient perception range and resolution, demonstrating significant advancement and effectiveness.
[0109] Example 3
[0110] This embodiment introduces a computer system, including:
[0111] Memory, for storing computer instructions;
[0112] A processor is configured to execute the computer instructions to implement the steps of the phase shift and time delay calculation method for a near-field synaesthesia integrated system as described in embodiment 1 or 2.
[0113] Example 4
[0114] This embodiment introduces a computer-readable storage medium having a computer program stored thereon. When the computer program is executed by a processor, the steps of the phase shift and time delay calculation method for a near-field synaesthesia integrated system described in Embodiment 1 or 2 are implemented.
[0115] Those skilled in the art will appreciate that the embodiments of the present application may be provided as methods, systems, or computer program products. Therefore, the present application may take the form of an entirely hardware embodiment, an entirely software embodiment, or an embodiment combining software and hardware. Furthermore, the present application may take the form of a computer program product implemented on one or more computer-usable storage media (including but not limited to magnetic disk storage, CD-ROM, optical storage, etc.) containing computer-usable program code.
[0116] The present application is described with reference to the flowcharts and / or block diagrams of the methods, devices (systems), and computer program products according to the embodiments of the present application. It should be understood that each process and / or block in the flowchart and / or block diagram, as well as the combination of processes and / or blocks in the flowchart and / or block diagram, can be implemented by computer program instructions. These computer program instructions can be provided to a processor of a general-purpose computer, a special-purpose computer, an embedded processor, or other programmable data processing device to produce a machine, so that the instructions executed by the processor of the computer or other programmable data processing device generate instructions for implementing the processes in the flowchart and / or block diagram. Figure 1one or more processes and / or blocks Figure 1 an apparatus for performing the functions specified in the flowchart or multiple flows and / or blocks.
[0117] These computer program instructions can also be stored in a computer readable memory that can direct a computer or other programmable data processing apparatus to function in a particular manner, such that the instructions stored in the computer readable memory produce an article of manufacture including instructions which implement the flowchart or multiple flows and / or blocks. Figure 1 one or more processes and / or blocks Figure 1 an apparatus for performing the functions specified in the flowchart or multiple flows and / or blocks.
[0118] These computer program instructions can also be loaded onto a computer or other programmable data processing apparatus to cause a series of operational steps to be performed on the computer or other programmable apparatus to produce a computer implemented process such that the instructions which execute on the computer or other programmable apparatus provide steps for implementing the flowchart or multiple flows and / or blocks. Figure 1 one or more processes and / or blocks Figure 1 an apparatus for performing the functions specified in the flowchart or multiple flows and / or blocks.
[0119] The embodiments of the present application described above are merely intended to illustrate the present application, and are not intended to limit the present application. The above-described embodiments are merely illustrative, and are not intended to limit the present application. Those skilled in the art can make many modifications without departing from the spirit and scope of the present application, and these modifications are also intended to be within the scope of the present application.
Claims
1. A phase shift and time delay calculation method for a near field communication integrated system, characterized in that, The method comprises the following steps: According to the preset system perception coverage, antenna spacing, system minimum frequency, system maximum frequency and system bandwidth, the phase shift of each phase shifter of the system and the initial time delay range of each time delay module are calculated; wherein, the preset system perception coverage comprises a preset perception angle domain coverage and a preset perception distance domain coverage; According to the preset system perception resolution, the preset system perception coverage, the antenna spacing, the system minimum frequency, the system maximum frequency and the system bandwidth, the final time delay range of each time delay module of the system is calculated; wherein, the preset system perception resolution comprises a preset perception angle domain resolution and a preset perception distance domain resolution; In the final time delay range, the time delay of each time delay module under the maximum communication user reachable rate is obtained; The phase shift of each phase shifter of the system is represented as: ; ; ; In the formula, denotes the phase shift of the phase shifter; denotes the lowest frequency of the system; denotes the speed of light; denotes the minimum spatial azimuth angle and the minimum spatial elevation angle in the preset system awareness coverage range, respectively; denotes the minimum spatial azimuth angle and the minimum spatial elevation angle in the preset system awareness coverage range, respectively; denotes the row index and the column index of the phase shifter, respectively; denotes the minimum spatial azimuth angle and the minimum spatial elevation angle in the preset system awareness coverage range, respectively; denotes the minimum spatial azimuth angle and the minimum spatial elevation angle in the preset system awareness coverage range, respectively; denotes the minimum distance in the preset system awareness coverage range; denotes the minimum physical azimuth angle in the preset system awareness coverage range; denotes the minimum physical elevation angle and the maximum physical elevation angle in the preset system awareness coverage range, respectively; denotes the minimum physical elevation angle and the maximum physical elevation angle in the preset system awareness coverage range, respectively. The initial time delay range of each time delay module of the system is represented as: ; Wherein, ; ; In the formula, represents the initial delay range of the first layer first delayer module; represents the initial delay range of the second layer first delayer module; and respectively represent the minimum delay that can be achieved by the first layer first delayer module and the second layer first delayer module; represents the highest frequency of the system; represents the antenna spacing; and respectively represent the minimum spatial azimuth angle and the maximum spatial azimuth angle within the preset system perceived coverage range; represents the lowest frequency of the system; represents the bandwidth of the system; and respectively represent the minimum spatial elevation angle and the maximum spatial elevation angle within the preset system perceived coverage range; and respectively represent the minimum distance and the maximum distance within the preset system perceived coverage range; The final time delay range of each time delay module of the system is represented as: ; Wherein, ; ; ; ; Where, Indicates the first layer The final delay range of each delay module; Indicates the second layer The final delay range of each delay module; and Represents the first layer The delay module and the second layer The maximum delay that can be achieved by a delay module; Indicates the highest frequency of the system; Indicates the antenna spacing; and They represent the minimum spatial orientation angle within the preset system perception coverage range and the maximum spatial orientation angle under the preset system perception resolution, respectively; and They represent the minimum distance within the preset system perception coverage range and the maximum distance under the preset system perception resolution respectively; Indicates the lowest frequency of the system; Indicates the system bandwidth; and They represent the minimum spatial pitch angle within the preset system perception coverage range and the maximum spatial pitch angle at the preset system perception resolution respectively; and They represent the maximum physical azimuth and maximum physical elevation angles under the preset system perception resolution respectively; The time delay of each time delay module under the maximum communication user reachable rate is represented as: ; ; Where, Indicates the first layer under the maximum achievable rate of communication users The delay of each delay module; Indicates the second layer under the maximum achievable rate of communication users The delay of each delay module; Indicates the highest frequency of the system; Indicates the antenna spacing; and Respectively represent the minimum spatial orientation angle and the maximum spatial orientation angle within the preset system perception coverage range; Indicates the lowest frequency of the system; Indicates the system bandwidth; and They represent the minimum and maximum spatial pitch angles within the preset system perception coverage range respectively; and They represent the minimum and maximum distances within the preset system perception coverage range respectively.
2. The method of claim 1, wherein, The preset system perception coverage is represented as: ; In the formula, represents the distance within the preset system perception coverage range; represents the physical azimuth angle within the preset system perception coverage range; represents the physical pitch angle within the preset system perception coverage range; and respectively represent the minimum distance and the maximum distance within the preset system perception coverage range; and respectively represent the minimum physical azimuth angle and the maximum physical azimuth angle within the preset system perception coverage range; and respectively represent the minimum physical pitch angle and the maximum physical pitch angle within the preset system perception coverage range.
3. The method of claim 1, wherein the method further comprises: calculating a phase shift and a time delay of the near field communication system. The preset system perception angle domain resolution is represented as: ; wherein, denotes the total number of subcarriers; denotes the subcarrier index; denotes the physical azimuth angle of the beam corresponding to the denotes the physical azimuth angle of the beam corresponding to the denotes the physical azimuth angle of the beam corresponding to the denotes the physical azimuth angle of the beam corresponding to the denotes the physical elevation angle of the beam corresponding to the denotes the physical elevation angle of the beam corresponding to the denotes the physical elevation angle of the beam corresponding to the denotes the physical elevation angle of the beam corresponding to the denotes the 3 decibel beamwidth.
4. The method of claim 1, wherein, The preset system perception distance domain resolution is represented as: ; wherein denotes the total number of subcarriers; denotes the subcarrier index; denotes the distance between the beam corresponding to the denotes the distance between the beam corresponding to the subcarrier and the beam corresponding to the subcarrier; denotes the 3 decibel beam depth; denotes the array aperture; denotes the wavelength; denotes the number of base station antennas; denotes the antenna spacing.
5. A computer system, characterized by The method comprises the following steps: A memory for storing computer instructions; A processor for executing the computer instructions to implement the steps of the phase shift and time delay calculation method for the near-field communication and perception integrated system according to any one of claims 1-4.
6. A computer-readable storage medium having stored thereon a computer program, characterized in that, The computer program is executed by the processor to implement the steps of the phase shift and time delay calculation method for the near-field communication and perception integrated system according to any one of claims 1-4.
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