带有关节相连的附属物的人造卫星姿态和形状轨迹跟踪控制

The Attitude and Shape Tracking Control of Satellite with Articulated Appendages

基于Chun le i R的研究工作,推导了建立在位形空间SO(3)×TM上带有关节相连附属物的人造卫星的姿态和形状跟踪控制的数学模型.针对该模型,设计了PD+适应补偿控制器,并进行了理论分析和试验仿真.

Based on the work of Chunlei R, deduce the mathematical model of attitude and shape control of satellite with articulated appendages, and the model define on the configure space SO（3）×T^dt, design PD and adaptive compensative controller. The credibility and availability of the proposed strategy is shown by theory and simulation.