期刊
ACTA ASTRONAUTICA
卷 55, 期 1, 页码 3-8出版社
PERGAMON-ELSEVIER SCIENCE LTD
DOI: 10.1016/j.actaastro.2003.12.012
关键词
-
The control problem of the spacecraft attitude using two momentum wheel actuators is investigated. It is well-known that attitude of a rigid spacecraft can be controlled by using three momentum wheels. If one of the momentum wheels is failure, the complete spacecraft equations are not controllable. When the total angular momentum of the system is zero, the control problem of the spacecraft attitude becomes a steering problem for a drift free control system. In this paper, based on the optimal control theory, a genetic algorithm for steering a rigid spacecraft with two momentum wheels is proposed. The genetic algorithm provide the results of a numerical simulation to prove its efficiency and stability. (C) 2004 Elsevier Ltd. All rights reserved.
作者
我是这篇论文的作者
点击您的名字以认领此论文并将其添加到您的个人资料中。
推荐
暂无数据