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Comprehensive test method of small satellite power subsystem

A technology for satellite power supply and comprehensive testing, which is applied in the direction of power supply testing, measuring power, and measuring devices. It can solve problems such as lack of operability, lack of test operation steps, and lack of detailed test content. The process is clear and detailed, and the test coverage is good

Active Publication Date: 2012-05-23
AEROSPACE DONGFANGHONG SATELLITE
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Problems solved by technology

[0004] In the Proceedings of the Space Energy Annual Conference of the Chinese Society of Astronautics published on December 1, 2002, a paper titled "Comprehensive Testing Technology for Space Power System" introduced the concept of comprehensive testing of the space power subsystem, listing Part of the test items for the comprehensive test of the space power supply subsystem, but there is no detailed test content, especially the lack of feasible test operation steps, and it is not operable

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  • Comprehensive test method of small satellite power subsystem
  • Comprehensive test method of small satellite power subsystem
  • Comprehensive test method of small satellite power subsystem

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Embodiment Construction

[0027] Such as figure 1 Shown is the composition principle of the small satellite power supply subsystem and the block diagram of the test system structure. The small satellite power supply subsystem is a fully regulated DC bus system with a distinction between charging arrays and power supply arrays, and is mainly composed of power controllers, battery packs, and solar cell arrays. The power controller includes a shunt regulation circuit, a charge regulation circuit, a charge / shunt controller, a discharge regulator and a power lower computer.

[0028] figure 1 Among them, solar battery array 1 and solar battery array 2 are only used to supply power for satellites, and cannot charge battery packs, which are called power supply array 1 and power supply array 2; solar battery array 3 to solar battery array 8 can not only supply power for satellites, but also Capable of charging the battery pack, called charging array 3 to charging array 8 . The charging regulating circuit 1 t...

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Abstract

The invention discloses a comprehensive test method of a small satellite power subsystem. In the method, a solar cell array is replaced by a solar matrix simulator; a ground wired test and control platform of a satellite comprehensive test system is used to transmit wired instructions and collect important parameters; and ground test and control equipment, a remote measurement and control front end and a test computer are used to transmit remote control instructions and collect remote test data. After the satellite is electrified, the on operation time, off operation time and remote control command transmission time of the solar matrix simulator are reasonably controlled, the working state of a power subsystem is set, various parameters and states are monitored and interpreted, and thus, various test items are accomplished. In addition, a method of injecting normal or fault data blocks and program blocks is adopted to test the up injection function, reliability and fault tolerance aretested. The method has high test coverage, clear and definite flow, simple and reliable operation and convenient construction.

Description

technical field [0001] The invention relates to a comprehensive test method for a fully-adjustable bus small satellite power supply subsystem which adopts a distinction between a charging array and a power supply array. Background technique [0002] It is generally believed that satellites with a mass of 500-1000Kg are small satellites. As the power generation device of the small satellite, the power subsystem is the energy source of the entire satellite. It is mainly composed of a power controller, a battery pack, and a solar array. The power controller is used to centrally realize the control functions of the satellite power subsystem, including bus voltage Regulation, solar cell array output power split control, battery charge and discharge control, and interface with other subsystems. The performance and functional characteristics of the power subsystem directly affect the working status and lifetime of other systems. [0003] Satellite comprehensive test means that af...

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Application Information

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Patent Type & Authority Patents(China)
IPC IPC(8): G01R31/02G01R31/36G01R31/40
Inventor 李立王建军陈逢田吴亚光程城
Owner AEROSPACE DONGFANGHONG SATELLITE
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