Abstract
Abstract A new adaptive control law design for moving mass control of a novel flight vehicle configuration is proposed. The coupling dynamic model between angle of attack and deflection angle is generated. An integrated control of attitude-servo system based on immersion and invariance (I&I) theory is presented to deal with the coupling caused by the additional inertia moment. To overcome the uncertainties in the model, the I&I theory is employed to design estimator to estimate the unknown aerodynamic parameters. The simulation results show that the proposed configuration is feasible and validate the quality of the adaptive controller.
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