Nonlinear six-degree-of-freedom control for flexible spacecraft

被引：0
|
作者：
Yamashita, T [1 ]
Uo, M [1 ]
Hashimoto, T [1 ]
机构：
[1] NEC Corp Ltd, Funct Devices Res Labs, Kawasaki, Kanagawa, Japan
来源：
AUTOMATIC CONTROL IN AEROSPACE 2001 | 2002年
关键词：
sliding-mode control; nonlinear control systems; position and attitude control; robust stability; phase plane;
D O I：
暂无
中图分类号：
TP [自动化技术、计算机技术];
学科分类号：
0812 ;
摘要：
A nonlinear six-degree-of-freedom control algorithm for flexible spacecraft has been developed. This algorithm consists of switching curves and control laws based on a sliding-mode control scheme. It can achieve both system stability and minimum fuel consumption simultaneously. The performance of the algorithm is assessed for the final-descent phase of MUSES-C spacecraft, and compared with that of a conventional control algorithm. Simulation results show that the proposed algorithm can improve total fuel consumption and time required for descending from the initial position to the surface of the asteroid. Copyright(C) 2001 IFAC.
引用
收藏
页码：327 / 332
页数：6
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