Attitude performance of the spacecraft combined energy and attitude control system

被引：0

作者：

Varatharajoo, R ^{[1
]}

Abdullah, MNF ^{[1
]}

机构：

[1] Univ Pertanian Malaysia, Dept Aerosp Engn, Selangor 43400, Malaysia

来源：

JBIS-JOURNAL OF THE BRITISH INTERPLANETARY SOCIETY | 2004年 / 57卷 / 7-8期

关键词：

onboard errors; attitude control; CEACS;

D O I：

暂无

中图分类号：

V [航空、航天];

学科分类号：

08 ; 0825 ;

摘要：

An attitude control architecture is proposed for the combined energy and attitude control system (CEACS), which operates in a speed control mode. The non-ideal CEACS attitude performance is deeply investigated herein. In this regard, numerical treatments are performed profoundly, and the most critical CEACS configuration on a spacecraft is identified.

引用

页码：237 / 241

页数：5

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