三轴零动量卫星在轨转偏置动量控制的设计与实现

doi:10.3969/j.issn.1674-1579.2013.02.001

›› 2013, Vol. 39 ›› Issue (2): 1-5.doi: 10.3969/j.issn.1674-1579.2013.02.001

Beijing Institute of Control Engineering, Beijing 100190, China

Online:2013-04-24 Published:2013-04-26

Abstract

Abstract: CBERS-2B satellite’s scheme was switched from zero-momentum control to biased-momentum control and magnetic control by uploading the control program to AOCC, when the main gyros were invalid. The implementation of biased-momentum control is described and the telemetry data analysis is supplied to evaluate the satellite’s flight. It was a successful experience for this kind of satellites to settle a stable flight with high reliability under the failure of crucial devices such as gyro, momentum wheel.

Key words: CBERS1, zero momentum control, biased momentum control, AOCC

CLC Number:

TP273

YUAN Jun, WEI Yi, WANG Zhe, WANG Shu-Yi, FU Xiu-Tao, WANG Xin-Min, WANG Sheng-Gang, ZHOU Jian-Min. Design and Implementation of Switching from Zero-Momentum Control to Biased-Momentum Control for Satellite Control System[J]., 2013, 39(2): 1-5.

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URL: http://journal01.magtech.org.cn/Jwk3_kjkzjs/EN/10.3969/j.issn.1674-1579.2013.02.001

http://journal01.magtech.org.cn/Jwk3_kjkzjs/EN/Y2013/V39/I2/1

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Design and Implementation of Switching from Zero-Momentum Control to Biased-Momentum Control for Satellite Control System

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