System test method for spacecraft docking flight mission
A technology for flight missions and system testing, applied in transmission systems, digital transmission systems, electrical components, etc., can solve problems such as poor authenticity, and achieve the effect of improving effectiveness and ensuring successful implementation.
Active Publication Date: 2018-08-17
BEIJING SPACE TECH RES & TEST CENT
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Problems solved by technology
[0004] The purpose of the present invention is to provide a system test method for spacecraft docking flight tasks, to solve the problem of poor authenticity in the system test process
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[0041] like figure 1 As shown, according to an embodiment of the present invention, a kind of system testing method for spacecraft docking mission of the present invention comprises:
[0042] S1. Build a test system for testing the docking flight mission of the spacecraft, and adjust the test system to the real flight mission state;
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Abstract
The invention relates to a system test method for a spacecraft docking flight mission. The method includes the following steps: S1, constructing a test system for testing a spacecraft docking flight mission, and adjusting the test system to a real flight mission state; and S2, testing the test system according to a test project. By really carrying various equipment in an spacecraft rendezvous anddocking mission through an astronaut system, a manned spacecraft system, a target spacecraft system and a measurement and control communication system, interfaces among the astronaut system, the manned spacecraft system, the target spacecraft system and the measurement and control communication system can be verified according to a real on-orbit flight mission, the effectiveness of various systemtests during the docking flight mission can be improved, and the successful implementation of an actual rendezvous and docking flight mission can be further ensured.
Description
technical field [0001] The invention relates to a system test method, in particular to a system test method for spacecraft docking missions. Background technique [0002] When performing manned rendezvous and docking flight missions, the astronaut system, manned spacecraft system, target spacecraft system, and measurement and control communication system need to cooperate to complete the rendezvous and docking of aircraft, on-orbit aircraft assembly information management, spaceflight Crews stay in orbit, space-ground integrated data transmission. In order to meet the flight mission requirements, each system is designed with an inter-system interface, which is used to realize information transmission between systems or provide mission support to other systems. [0003] During the full-cycle product development process of each system, the correctness of product design status will be tested and verified at different development stages such as stand-alone level, sub-system lev...
Claims
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Patent Type & Authority Applications(China)
IPC IPC(8): H04L12/26
CPCH04L43/50
Inventor 王志莹杨宏何宇李卫程伟南洪涛陈丹王丹郭中伟
Owner BEIJING SPACE TECH RES & TEST CENT
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