Abstract：A new approach combined adaptive robust method and theory is proposed for active vibration control of a flexible spacecraft during attitude maneuver control．For effective vibration suppression in flexible appendages, the controller based on state feedback theory is used and the structural uncertainties caused by neglecting higher order modes are fully considered in the design procedure, which ensures the rapid decay of the vibration and the robustness. Then, adaptive robust method which can reduce the influences of disturbances and uncertainties of moment of inertia is applied to develop the attitude controller of the spacecraft and the Lyapunov theory is introduced to prove the system stability. Finally, the reasonability and effectiveness of the proposed method is testified via the simulation.
袁国平;史小平;李隆 . 航天器姿态机动的自适应鲁棒控制及主动振动抑制[J]. , 2013, 32(12): 110-115.
YUAN Guo-ping SHI Xiao-ping LI Long. Adaptive Robust Attitude Maneuver Control of Flexible Spacecraft with Active Vibration Suppression. , 2013, 32(12): 110-115.
2013, Vol. 32 
