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Low-orbit constellation phased array communication navigation fusion application terminal

A technology that integrates applications and low-orbit constellations, applied in the field of electricity

Active Publication Date: 2022-05-17
BEIJING RES INST OF TELEMETRY +1
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0008] The present invention aims to solve the application problem of orbital constellation communication and navigation fusion, and provides a low-orbit constellation phased array communication and navigation fusion application terminal, which integrates antennas, amplifiers, radio frequency channels, baseband processing, and power supplies. By receiving and processing GNSS navigation signals, fusion Measured terminal three-dimensional acceleration and three-dimensional angular velocity information, real-time calculation of terminal position and attitude information, and provide communication satellite pitch angle and azimuth information for digital phased array processing, using digital phased array beamforming technology to receive multiple low-orbit satellites Satellite communication information, using digital phased array weighted modulation technology to send communication information to low-orbit satellites, completing the two-way communication function of low-orbit satellites

Method used

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  • Low-orbit constellation phased array communication navigation fusion application terminal
  • Low-orbit constellation phased array communication navigation fusion application terminal
  • Low-orbit constellation phased array communication navigation fusion application terminal

Examples

Experimental program
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Effect test

Embodiment 1

[0080] like figure 1 As shown, a low-orbit constellation phased array communication and navigation fusion application terminal includes an array antenna unit 1, an amplifier unit 2, a radio frequency channel unit 3, a baseband processing unit 4, an interface unit 5, and an amplifier unit 2, The radio frequency channel unit 3, the baseband processing unit 4, and the interface unit 5 are all electrically connected to the power supply unit 6, and the baseband processing unit 4 is used for GNSS navigation signal, fusion application terminal position information, fusion application terminal attitude information, beam pointing pitch angle, The azimuth angle of the beam pointing, the relative position of the antenna element and the phase zero value of the beam formation are calculated to obtain the phase shift value of the array antenna element 1 for navigation enhancement;

[0081] The array antenna unit 1 includes a GNSS antenna 11 and a communication antenna 12 arranged in an arra...

Embodiment 2

[0104] like figure 1 As shown, a low-orbit constellation phased array communication and navigation fusion application terminal, the device is a communication and navigation fusion application terminal equipment for GNSS signals and low-orbit satellite signals, including an antenna unit 1, an amplifier unit 2, a radio frequency channel unit 3, a baseband The processing unit 4 , the interface unit 5 and the power supply unit 6 ; the power supply unit 6 supplies power to the amplifier unit 2 , the radio frequency channel unit 3 , the baseband processing unit 4 and the interface unit 5 .

[0105] The antenna unit 1 includes a 2-element GNSS receiving antenna 11 and a 20-element communication antenna 12 . The GNSS antenna is used to receive GNSS navigation signals; the communication antenna 12 is used to receive and transmit low-orbit satellite signals.

[0106] The amplifier unit 2 includes 2 channels of GNSS low noise amplifiers, 20 channels of communication low noise amplifiers...

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Abstract

The invention provides a low-orbit constellation phased array communication and navigation fusion application terminal, which integrates an antenna, an amplifier, a radio frequency channel, baseband processing and a power supply, integrates measured terminal three-dimensional acceleration and three-dimensional angular velocity information by receiving and processing GNSS navigation signals, solves terminal position and attitude information in real time, and realizes communication and navigation. The low-earth-orbit satellite two-way communication method comprises the steps of receiving a plurality of low-earth-orbit satellites, providing pitch angle and azimuth angle information of the communication satellites for digital phased array processing, receiving communication information of the low-earth-orbit satellites by adopting a digital phased array beam forming technology, sending the communication information to the low-earth-orbit satellites by adopting a digital phased array weighted modulation technology, and completing a low-earth-orbit satellite two-way communication function. According to the invention, the integrated design of each module is realized in a relatively small volume, attitude measurement based on satellite navigation and inertia combination is completed, an accurate reference is provided for beam pointing, receiving and transmitting digital beam processing of low-orbit communication radio frequency signals is completed, and the function of supporting communication access of two low-orbit satellites at the same time is realized.

Description

technical field [0001] The invention relates to the technical field of electricity, in particular to a low-orbit constellation phased array communication and navigation fusion application terminal. Background technique [0002] Low-orbit satellites are often used as communication satellites because they are close to the ground, have excellent signal quality, and have a smaller time delay. The low-orbit satellite constellation can provide information enhancement and signal enhancement to the navigation constellation on a global scale, provide users with real-time high-precision positioning services, and improve the efficiency of communication and remote sensing services. LEO constellations have gradually attracted the attention and favor of academia and industry due to their unique advantages of both communication and navigation functions. [0003] The US Iridium system and the GPS system jointly developed a new type of satellite timing and positioning service (STL), which h...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): H04B7/185G01S19/42
CPCH04B7/18513H04B7/18519G01S19/42Y02D30/70
Inventor 蒋林朱懋华季海福李绍华张婉婷
Owner BEIJING RES INST OF TELEMETRY
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