Velocity-free attitude tracking control of rigid spacecrafts under control constraints

被引:0
作者
Li, Chuanjiang [1 ]
Ma, Guangfu
Song, Bin
机构
[1] Harbin Inst Technol, Dept Control Sci & Engn, Harbin 150001, Peoples R China
[2] Harbin Inst Technol, Grad Sch, Harbin 150001, Peoples R China
来源
DYNAMICS OF CONTINUOUS DISCRETE AND IMPULSIVE SYSTEMS-SERIES B-APPLICATIONS & ALGORITHMS | 2007年 / 14卷
关键词
attitude tracking; spacecraft; output feedback; MRP vector; control saturations; lyapunov method;
D O I
暂无
中图分类号
O29 [应用数学];
学科分类号
070104 ;
摘要
This paper considers the output feedback, attitude tracking control of rigid spacecrafts subject to the absence of angular velocity measurements and control saturations. It is assumed that only attitude measurement, which is represented by Modified Rodrigues Parameter (MRP), is available for feedback. A stable filter driven by the attitude variable is adopted to reconstruct velocity-like signals. The proposed control scheme is shown to achieve global asymptotic attitude tracking through a rigorous Lyapunov analysis, with an adoption of. a particular non-quadratic Lyapunov function. Numerical simulations demonstrate the practical applicability of the proposed approach.
引用
收藏
页码:82 / 86
页数:5
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