Design and robust analysis for spacecraft attitude controller

Zhou Fengqi; Han Yanhua; Zhou Jun

Design and robust analysis for spacecraft attitude controller

Zhou Fengqi
, Han Yanhua
, Zhou Jun

航天学院

Northwestern Polytechnical University Xian

科研成果: 期刊稿件 › 文章 › 同行评审

2 引用（Scopus）

摘要

The spacecraft's attitude control system was divided into the outer loop that was angle loop and the inner loop that was angle velocity loop based on their time scales. Then the control law of each loop was designed independently using exact linearization method. In the inner loop, robust stability was analysed using small-gain theorem considering the existence of perturbation of spacecraft moment inertia.

源语言	英语
页（从-至）	36-41
页数	6
期刊	Zhongguo Kongjian Kexue Jishu/Chinese Space Science and Technology
卷	27
期	2
出版状态	已出版 - 4月 2007

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title = "Design and robust analysis for spacecraft attitude controller",

abstract = "The spacecraft's attitude control system was divided into the outer loop that was angle loop and the inner loop that was angle velocity loop based on their time scales. Then the control law of each loop was designed independently using exact linearization method. In the inner loop, robust stability was analysed using small-gain theorem considering the existence of perturbation of spacecraft moment inertia.",

keywords = "Exact linearization, Robust control attitude control, Singular perturbation, Small-gain theorem, Vehicle",

author = "Zhou Fengqi and Han Yanhua and Zhou Jun",

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AU - Jun, Zhou

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AB - The spacecraft's attitude control system was divided into the outer loop that was angle loop and the inner loop that was angle velocity loop based on their time scales. Then the control law of each loop was designed independently using exact linearization method. In the inner loop, robust stability was analysed using small-gain theorem considering the existence of perturbation of spacecraft moment inertia.

KW - Exact linearization

KW - Robust control attitude control

KW - Singular perturbation

KW - Small-gain theorem

KW - Vehicle

UR - https://www.scopus.com/pages/publications/34250617490

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SN - 1000-758X

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Design and robust analysis for spacecraft attitude controller

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