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Aerostat-based occultation detection system and method

A detection system and processor technology, applied in the field of space detection, can solve the problems of inability to achieve key observations in key areas, less allocation of occultation channels, and high launch costs, and achieve the effect of real-time and flexible configuration

Pending Publication Date: 2018-12-14
CMA METEOROLOGICAL OBSERVATION CENT +1
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0003] In the process of realizing the present invention, the inventor found that the existing technology has the disadvantages of less allocation of occultation channels, heavy weight, high launch cost, and failure to realize key observations in key areas. Domestically, GNSS occultation detection is lightweight, low-cost, and Multi-purpose research is still in the preliminary research stage, with less relevant information, far behind the research level of NASA (National Aeronautics and Space Administration, National Aeronautics and Space Administration) and ESA (European Space Agency, European Space Agency)

Method used

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  • Aerostat-based occultation detection system and method

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Embodiment 1

[0050] figure 1 A structural block diagram of an aerostat-based occultation detection system provided for Embodiment 1 of the present invention. This embodiment can be applied to quickly switch between ionospheric occultation detection and atmospheric occultation detection functions through telemetry commands to achieve real-time and flexible Configure the occultation channel to focus on the observation of key areas. Such as figure 1 As shown, the system includes:

[0051] GNSS occultation antenna array 110 , GNSS direct antenna 120 , radio frequency signal processing circuit 130 , digital signal processing circuit 140 , antifuse FPGA 150 and FLASH memory 160 .

[0052] It should be noted that the occultation detection system provided by the embodiment of the present invention can be configured on an aerostat to realize the above-mentioned occultation detection function, wherein, in particular, the aerostat can be an airship (near-space airship or space airship )Wait. Typi...

Embodiment 2

[0068] Such as Figure 2a As shown, in this embodiment, a specific structural block diagram of an aerostat-based occultation detection system is given.

[0069]In the embodiment of the present invention, optionally, based on the above-mentioned occultation detection system, the radio frequency signal processing circuit specifically includes: a GNSS occultation radio frequency signal processing subcircuit 131 and a GNSS direct radio frequency signal processing subcircuit 132 .

[0070] The GNSS occultation radio frequency signal processing subcircuit 131 is connected to the GNSS occultation antenna array 110 and the digital signal processing circuit 140 respectively, and the GNSS direct radio frequency signal processing subcircuit 132 is connected to the GNSS direct antenna 120 and the digital signal processing subcircuit 132 respectively. The processing circuit 140 is connected, and the GNSS occultation radio frequency signal processing sub-circuit 131 and the GNSS direct radi...

Embodiment 3

[0088] image 3 It is a flow chart of an aerostat-based occultation detection method provided in Embodiment 3 of the present invention, which is applied to the aerostat-based occultation detection system described in any embodiment of the present invention. This embodiment is applicable to the situation where the ground telemetry bus command is received through the antifuse FPGA, bit stream files with different functions are selected to be loaded to the SOC processor by analyzing the command, and the functions of ionospheric occultation detection and atmospheric occultation detection are quickly switched. Such as image 3 As shown, the method includes:

[0089] Step 310, acquiring and analyzing ground telemetry instructions;

[0090] In this embodiment, when a power-on start command is detected, the antifuse FPGA acquires the ground telemetry command and performs command analysis on the ground telemetry command.

[0091] Step 320, according to the command analysis result, l...

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Abstract

Embodiments of the invention disclose an aerostat-based occultation detection system and method. The system comprises a GNSS occultation antenna array, a GNSS through antenna, a radio frequency signalprocessing circuit, a digital signal processing circuit, an anti-fuse FPGA and a FLASH memory; the GNSS occultation antenna array is connected with the radio frequency signal processing circuit; theGNSS through antenna is connected with the radio frequency signal processing circuit; the radio frequency signal processing circuit is connected with the digital signal processing circuit; the digitalsignal processing circuit is connected with the anti-fuse FPGA; the anti-fuse FPGA is connected with the FLASH memory; and the FLASH memory is used for storing a bit stream file. According to the technical scheme provided by the embodiment of the invention, the bit stream files with different functions are loaded to an SOC processor by analyzing the telemetering instructions, an ionized layer mask occultation function and an atmospheric occultation detection function are rapidly switched, and key observation is carried out on the key region.

Description

technical field [0001] Embodiments of the present invention relate to space detection technology, in particular to an aerostat-based occultation detection system and method. Background technique [0002] In recent years, GNSS (Global Navigation Satellite System, Global Navigation Satellite System) has developed rapidly in countries all over the world. Among them, the aerospace industry has entered the process of commercialization in many fields, and the application of GNSS remote sensing technology has made breakthrough progress. GNSS remote sensing technology uses radio waves to propagate in the earth's atmosphere, or changes in signal amplitude, phase and other physical quantities after being reflected by ground objects, to invert meteorological elements such as the earth's atmosphere, ocean and soil. The retrieval products of GNSS occultation detection are ionosphere and atmospheric parameters. Ionospheric inversion products include ionospheric electron density profile a...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): G01S19/14G01S19/37G01S19/36
CPCG01S19/14G01S19/36G01S19/37
Inventor 郭启云杨荣康李昌兴王鹏程黄满义张春泽
Owner CMA METEOROLOGICAL OBSERVATION CENT
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