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Radiation electromagnetic compatibility test method for electric propulsion system and on-star radio frequency equipment

A technology of electromagnetic compatibility and test method, which is applied in the direction of measuring electricity, measuring electrical variables, measuring devices, etc., to achieve the effects of easy implementation, cost saving, and reduction of test complexity

Active Publication Date: 2012-01-18
AEROSPACE DONGFANGHONG SATELLITE
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  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0006] The technical problem solved by the present invention is: to overcome the difficulty of not having an electromagnetic compatibility testing laboratory for electric propulsion systems, and to provide a simple and easy-to-implement test method for electromagnetic compatibility between electric propulsion systems and on-board radio frequency equipment radiation

Method used

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  • Radiation electromagnetic compatibility test method for electric propulsion system and on-star radio frequency equipment
  • Radiation electromagnetic compatibility test method for electric propulsion system and on-star radio frequency equipment
  • Radiation electromagnetic compatibility test method for electric propulsion system and on-star radio frequency equipment

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Embodiment Construction

[0028] The method mainly includes the radiation susceptibility test of the transponder and the radiation susceptibility test of the GPS receiver.

[0029] Schematic diagram of radiation susceptibility test of transponder figure 1 As shown, the whole system consists of electric propulsion system (ion power supply module, propellant storage and supply unit, digital interface and control module, ion thruster module), TS-6 vacuum system (main vacuum tank, air pumping system), wave-transparent auxiliary Cabin, control computer, transponder, remote control unit, satellite computer, measurement and control ground equipment, ground measurement and control antenna, transponder antenna, satellite structure, wave-absorbing material board, etc.

[0030] The electric propulsion system consists of a xenon ion thruster (including thruster bracket), a set of ion power supply, a set of propellant storage and supply unit, a set of digital interface and control module. The relationship between ...

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Abstract

The invention discloses a radiation electromagnetic compatibility test method for an electric propulsion system and on-star radio frequency equipment. Firstly, an ion thruster is arranged in a wave transmitting secondary cabin; the wave transmitting secondary cabin is connected with a main vacuum tank; and electromagnetic radiation interference produced by a plume of the ion thruster is emitted out of the main vacuum tank through the wave transmitting secondary cabin. Each equipment and antenna are connected. When the electric propulsion system is started to normally work, both uplink level and downlink level of a responder are weak levels; conditions of uplink instruction reception and downlink remote metering error code are checked; if the instruction reception is correct, the code ratemeets the requirement and the responder is not interfered; remote metering parameters for a GPS (Global Positioning System) receiver are observed, and absolute positioning condition and relative positioning condition are determined; and if the remote metering is correct and the positioning is normal, the GPS receiver is not interfered.

Description

technical field [0001] The invention relates to an electromagnetic compatibility test method of an electric propulsion system, in particular to a radiation electromagnetic compatibility test method of the electric propulsion system and on-board radio frequency equipment. Background technique [0002] Since the satellite electric propulsion system has high voltage, high current, large voltage or current change rate, and complex plasma environment, the radiation emission electromagnetic interference generated by the electric propulsion system will cause serious damage to the radio frequency equipment on the satellite. potential impact. These radiated electromagnetic interferences may come from the power distribution management unit (PPU), cables, electric thrusters, and emissions in the extraction plume. The electric propulsion system and the on-board radio frequency equipment must ensure electromagnetic compatibility, so the radiation electromagnetic compatibility verificati...

Claims

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Application Information

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IPC IPC(8): G01R31/00
Inventor 杨争光高杰李冉崔铁民吴璇叶扬
Owner AEROSPACE DONGFANGHONG SATELLITE
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