SLIDING MODE OBSERVER FOR SPACECRAFT ATTITUDE ESTIMATION: A SPECIAL CASE

被引：0

作者：

Aly, Mohamed M. ^{[1
]}

Fatah, Hossam Eldin-A. Abdel ^{[2
]}

Bahgat, Ahmed ^{[2
]}

机构：

[1] Old Dominion Univ, Dept Aerosp Engn, Norfolk, VA 23529 USA

[2] Cairo Univ, Dept Elect Engn, Giza 12611, Egypt

来源：

ASTRODYNAMICS 2009, VOL 135, PTS 1-3 | 2010年 / 135卷

关键词：

D O I：

暂无

中图分类号：

P1 [天文学];

学科分类号：

0704 ;

摘要：

This paper presents a sliding mode observer (SMO), that can be used for moderate-accuracy attitude determination systems for LEO Earth-pointing spacecraft (s/c), which is typically using Gyroscopes, Earth, and Sun sensors for attitude sensing, this is to provide a substitute for the yaw data in case of the s/c eclipse periods or limited field of views. The nonlinear observability for this system is investigated analytically via the calculation of Lie derivatives to check the possibility of the system states estimation. The performance of the SMO observer is presented, the stability for the SMO is proven and SMO enhanced estimates is shown.

引用

页码：1417 / +

页数：3

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