Abstract:

A method for design of the novel adaptive sliding mode observer and its corresponding controller is proposed for momentum biased satellite at titude tracking control with unknown measure yaw attitude. The smooth sliding mode observer is designed by using roll and pitch information so as to improve the state estimation robustness while suppressing high-frequency chattering. A proportional and integral sliding mode surface is proposed to implement an integral sliding mode control which could mitigate the steady-state error and optimize the global robustness of sliding mode. With purpose of compensating the passive effect of uncertain parameters, an adaptive update law is presented based on an adaptive method. Numerical simulation results show that, compared with Luenberger observer, the proposed method could improve the yaw attitude estimation accuracy and improve the pitch-yaw axis tracking precision by 50% as well as the guaranty of the robustness.