Satellite Attitude Tracking Control under Control Saturation
The main problem addressed is Modified Rodrigues Parameter (MRP) based, attitude tracking control of rigid satellite. First a nonlinear control scheme is presented under control input saturation. The control scheme is shown to achieve global asymptotic stability for the whole tracking error states through a rigorous Lyapunov analysis. Then we give a control scheme not only to deal with the control input saturation but also error angular velocity constraints, and a detail stability analysis of the closed-loop is included. Numerical simulations are performed for the satellite attitude tracking control system and results demonstrate the effective of the proposed control schemes.
Jianting Lv Dai Gao Xibin Cao
School of Astronautics,Harbin Institute of Technology;School of Mathematical Science,Heilongjiang Un School of Astronautics,Harbin Institute of Technology
国际会议
深圳
英文
994-998
2008-12-10(万方平台首次上网日期,不代表论文的发表时间)