委内瑞拉遥感卫星姿轨控系统方案及在轨验证

doi:10.3969/j.issn.1674-1579.2013.05.010

Abstract

Abstract: The attitude and orbit control system of VRSS1 satellite is introduced， including main functions， required specifications， system composition， work modes， control strategy design and main failure diagnosis logic． According to operation data of the satellite on orbit， some operation results and the performance are presented． Furthermore，the attitude and orbit control system scheme is demonstrated on orbit．

Key words: VRSS1 satellite, attitude and orbit control system scheme, onorbit test

CLC Number:

V448.2

ZENG Chun-Ping, LIU Qi-Rui, DONG Jun. Attitude and Orbit Control System Design and Onorbit Test of VRSS1 Satellite[J]., 2013, 39(5): 48-52.

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URL: http://journal01.magtech.org.cn/Jwk3_kjkzjs/EN/10.3969/j.issn.1674-1579.2013.05.010

http://journal01.magtech.org.cn/Jwk3_kjkzjs/EN/Y2013/V39/I5/48

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Attitude and Orbit Control System Design and Onorbit Test of VRSS1 Satellite

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