Transactions of Nanjing University of Aeronautics & Astronautics
Robust Adaptive Attitude Maneuvering and Vibration Reducing Control of Flexible Spacecraft Under Input Saturation
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Abstract:
A robust adaptive control scheme is proposed for attitude maneuver and vibration suppression of flexible spacecraft in situations where parametric uncertainties, external disturbances, unmeasured elastic vibration and input saturation constraints exist. The controller does not need the knowledge of modal variables but the estimates of modal variables provided by appropriate dynamics of the controller. The requirements to know the system parameters and the bound of the external disturbance in advance are also eliminated by adaptive updating technique. Moreover, an auxiliary design system is constructed to analyze and compensate the effect of input saturation, and the state of the auxiliary design system is applied to the procedure of control design and stability analysis. Within the framework of the Lyapunov theory, stabilization and disturbance rejection of the overall system are ensured. Finally, simulations are conducted to study the effectiveness of the proposed control scheme, and simulation results demonstrate that the precise attitude control and vibration suppression are successfully achieved.
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Clc Number:
V448.22
CHINA AERO-SCIENCES
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