標題: SLIDING-MODE CONTROLLER-DESIGN FOR SPACECRAFT ATTITUDE TRACKING MANEUVERS
作者: CHEN, YP
LO, SC
交大名義發表
電控工程研究所
National Chiao Tung University
Institute of Electrical and Control Engineering
公開日期: 1-十月-1993
摘要: This paper presents a robust sliding-mode control law to deal with the spacecraft attitude tracking problems. Two important natural properties related to the spacecraft model of motion are shown and then by using these properties and the second method of Lyapunov theory, the system stability in the sliding mode can be easily achieved. The success of the sliding-mode controller and the robustness to uncertainties are illustrated by an example of multiaxial attitude tracking maneuvers.
URI: http://dx.doi.org/10.1109/7.259536
http://hdl.handle.net/11536/2831
ISSN: 0018-9251
DOI: 10.1109/7.259536
期刊: IEEE TRANSACTIONS ON AEROSPACE AND ELECTRONIC SYSTEMS
Volume: 29
Issue: 4
起始頁: 1328
結束頁: 1333
顯示於類別:期刊論文


文件中的檔案:

  1. A1993MD77700025.pdf