Optimal control of a programmed motion of a rigid spacecraft using redundant kinematics parameterizations

被引：8
|
作者：
El-Gohary, A
机构：
[1] King Saud Univ, Fac Sci, Dept Stat & OR, Riyadh 11451, Saudi Arabia
[2] Mansoura Univ, Fac Sci, Dept Math, Mansoura 35516, Egypt
来源：
CHAOS SOLITONS & FRACTALS | 2005年 / 26卷 / 04期
关键词：
D O I：
10.1016/j.chaos.2005.02.036
中图分类号：
O1 [数学];
学科分类号：
0701 ; 070101 ;
摘要：
This paper considers the problem of optimal controlling of a programmed motion of a rigid spacecraft. Given a cost of the spacecraft as a quadratic function of state and control variables we seek for optimal control laws as functions of the state variables and the angle of programmed rotation that minimize this cost and asymptotically stabilize the required programmed motion. The stabilizing properties of the proposed controllers are proved using the optimal Liapunov techniques. Numerical simulation study is presented. (c) 2005 Elsevier Ltd. All rights reserved.
引用
收藏
页码：1053 / 1063
页数：11
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