Variable structure control of spacecraft reorientation maneuvers
暂无分享,去创建一个
A Variable Structure Control (VSC) approach is presented for multi-axial spacecraft reorientation maneuvers. A nonlinear sliding surface is proposed which results in an asymptotically stable, ideal linear sliding motion of Cayley-Rodriques attitude parameters. By imposing a desired equivalent dynamics on the attitude parameters, the approach is devoid of optimal control considerations. The single axis case provides a design scheme for the multiple axes design problem. Illustrative examples are presented.
[1] J. A. Breakwell,et al. Optimal feedback slewing of flexible spacecraft , 1981 .
[2] Bong Wie,et al. Quaternion feedback for spacecraft large angle maneuvers , 1985 .
[3] Yuan-Yih Hsu,et al. Optimal control of electric power generation using varible structure controllers , 1983 .
[4] T. A. W. Dwyer,et al. Exact nonlinear control of spacecraft slewing maneuvers with internal momentum transfer , 1984 .