Adaptive Tracking Control of Spacecraft Using Magnetic Actuators

摘要：

The attitude tracking control problem of the spacecraft using magnetic actuators is considered in this paper. We design the adaptive control law, which incorporates a velocity-generating filter from attitude measurement, to ensure the asymptotic convergence of the attitude and angular velocity tracking errors despite unknown spacecraft inertia. Simulation results demonstrate the practical applicability of the proposed approach.

作者: Zexin Guan Zhonghua Wang

作者单位: School of Control Science and Engineering, University of Jinan, China

会议类型: 国际会议

会议名称: The Second International Joint Conference on Computational Science and Optimization(CSO 2009)(2009 国际计算科学与优化会议)

会议地点: 三亚

会议语种:英文

页码: 1726-1729

在线出版日期: 2009-04-24（万方平台首次上网日期，不代表论文的发表时间）