Abstract
This paper proposes a tracking control strategy for a reconfigurable flight array system with varible configuration. The presented control scheme does not dependent on the accurate mathematical model of system. By employing a pseudo-inverse method with the control efficiency matrix, an control allocation method is constructed to achieve trajectory tracking for a multi-configuration flight array system. To maintain the trajectory tracking performance, an adaptive integral sliding mode controller is designed by using the distance information of the sliding variables and the boundary layer. Theoretical analysis is studied in terms of the Lyapunov theory. Finally, comparative simulation results are provided to demonstrate the effectiveness of the proposed method.
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