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.
Satellite attitude tracking control under control saturation
2008-12-01
509851 byte
Conference paper
Electronic Resource
English
Satellite attitude tracking controller design subject to control saturation
Tema Archive | 2007
|Adaptive Spacecraft Attitude Tracking Control with Actuator Saturation
Online Contents | 2010
|