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A new kind of robust adaptive control method is proposed for hypersonic vehicle with strong coupled characteristics and modeling uncertainties. Firstly, based on the founded dynamic model of hypersonic vehicle, the new coupling mathematical model with non-matched characteristics by introducing expected reference model. Secondly, the robust adaptive control strategy is derived by dynamical timely adjusting parameters and utilizing the solution of the Riccati equation. Finally, an illustrative example is given to show the proposed control scheme can guarantee the stability of the hypersonic vehicle under the condition of large-scale variation of model parameter perturbation and disturbance. [ABSTRACT FROM AUTHOR]

A mobile satellite communication system is installed on a moving carrier for satellite communication. The tracking and stabilizing problem of the mobile satellite communication system is studied in this paper. The tri-axis nonlinear model of the mobile satellite communication system is chosen as the control object, because it can describe the kinematics and dynamics features of the system more accurately than the single-axis model. Based on the actuator dynamic features, a nonlinear robust controller with actuator dynamic compensation is designed. The designed controller can eliminate the disturbances when the carrier is moving and track the target satellite accurately. Because the problem of the actuator dynamics is further considered, the controller is more suitable for the practical application. At last, three sets of comparative simulation results are used to verify the tracking and stabilizing effectiveness of the designed controller under different disturbances. [ABSTRACT FROM AUTHOR]