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Avionics system automatic test platform based on reusable spacecraft

A technology of automated testing and avionics systems, applied in the direction of electrical testing/monitoring, etc., can solve problems such as low automation and intelligence, insufficient openness and flexibility, and heavy testing workload, achieving strong versatility and flexibility performance, solving distributed remote testing problems, and high testing efficiency

Inactive Publication Date: 2013-02-06
CHINA ACAD OF LAUNCH VEHICLE TECH
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  • Abstract
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AI Technical Summary

Problems solved by technology

At present, there are some shortcomings in the spacecraft avionics comprehensive test system: there are many adapters in each subsystem, and the versatility is not strong; Sexuality and flexibility are not strong enough

Method used

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  • Avionics system automatic test platform based on reusable spacecraft
  • Avionics system automatic test platform based on reusable spacecraft

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Embodiment Construction

[0014] The present invention will be further introduced below in conjunction with the accompanying drawings.

[0015] The automatic test platform of reusable spacecraft avionics integrated system is a platform with complex technology and large scale. In the electrical performance test, the test platform needs to complete various signal detection, state control, measurement and testing, parameter monitoring, test process management, time reference, data recording and archiving, and support for testing equipment activities, etc. for the spacecraft; Realize various simulation, excitation and simulation functions. The automated test platform includes master control equipment with strong processing capabilities, which is used to realize automatic comprehensive management of the entire platform, and also includes various types of special test equipment, which are used to realize the detection of each subsystem of the reusable spacecraft. The reusable spacecraft avionics integrated ...

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Abstract

The invention discloses an avionics system automatic test platform based on a reusable spacecraft, which comprises an interface adapter, special test equipment, a photoelectric isolation network and a test terminal. According to the characteristics that the spacecraft has many subsystems and the subsystems are distributed dispersedly, the avionics system automatic test platform based on the reusable spacecraft unifies the adapter of the comprehensive test platform, reduces the types of ground equipment, realizes functional modularization of each system and integration of the system structure, and can automatically generate and change input signals or excitation sources, automatically control the on and off of input and output of a tested object, automatically measure and record output signals, automatically process test data, automatically interpret the work state of test equipment, automatically execute test program and automatically judge the test data so as to shorten the construction time of a test system and solve the problem about distributed remote test. The test system has high generality, flexibility and test efficiency, reduces the workload of testers and improves the test quality and the test efficiency.

Description

technical field [0001] The invention relates to an automated testing platform, in particular to an automated testing platform for an avionics system based on a reusable spacecraft, belonging to the field of automated testing. Background technique [0002] In the research of aerospace technology at home and abroad, reusable spacecraft is a complex system, and almost every stage of its design and development is inseparable from testing. Through the test, the design and production process defects of the spacecraft can be fully exposed, the early failure of electronic components and the lack of software can be found, and the quality of the aircraft product can be ensured. [0003] The spacecraft electrical integrated system (abbreviated as the avionics integrated system) includes navigation, guidance and control (GNC) system, measurement and control communication subsystem, data management subsystem, power supply and power distribution subsystem, health management subsystem and ...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): G05B23/02
Inventor 刘旭东徐海运高祥武
Owner CHINA ACAD OF LAUNCH VEHICLE TECH
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