A correction method of spin-stabilized satellites attitude control based on infrared benchmark

Zhou Jinbiao; Li Yonggang; Guo Libing; Li Xiangming; Mao Wen

doi:10.16157/j.issn.0258-7998.190675

Dianzi Jishu Yingyong (Sep 2019)

A correction method of spin-stabilized satellites attitude control based on infrared benchmark

Zhou Jinbiao,
Li Yonggang,
Guo Libing,
Li Xiangming,
Mao Wen

Affiliations

Zhou Jinbiao: Trainee Team 2 of the 49th Joint Operational Command Training Course of National Defense University，Beijing 100091，China
Li Yonggang: China Satellite Maritime Tracking and Control Department，Jiangyin 214431，China
Guo Libing: China Satellite Maritime Tracking and Control Department，Jiangyin 214431，China
Li Xiangming: China Satellite Maritime Tracking and Control Department，Jiangyin 214431，China
Mao Wen: China Satellite Maritime Tracking and Control Department，Jiangyin 214431，China

DOI: https://doi.org/10.16157/j.issn.0258-7998.190675
Journal volume & issue: Vol. 45, no. 9
pp. 93 – 96

Abstract

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Aiming at the problem that there is a large deviation of the spin-stabilized satellite using infrared benchmark for attitude controlling, the control theory of isoclinic angle is described firstly, the difference between the solar reference and infrared benchmark on attitude controlling is analyzed，the main cause leading to the large deviation using infrared benchmark is also explained. A method of execution angle compensation and correction is put forward finally. Verified by simulation, the control precision is improved effectively after execution angle correction.

Published in Dianzi Jishu Yingyong

ISSN: 0258-7998 (Print)
Publisher: National Computer System Engineering Research Institute of China
Country of publisher: China
LCC subjects: Technology: Electrical engineering. Electronics. Nuclear engineering: Electronics
Website: http://journal.chinaaet.com/en

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