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Asymmetric structure damage such as loss of wing tip can cause unknown changes to the aircraft mass, center of gravity and aerodynamic characteristics, which will make the whole system becomes difficult to control. Aiming at this problem, this paper presents a robust fault-tolerant control strategy based on nonlinear extended state observer and gain preset PID (Proportion Integration Differentiation)...
This paper focuses on the control problem of the aircraft with asymmetric structure damage. The contribution of this study is to present a new robust fault-tolerant control strategy based on nonlinear extended state observer and nonlinear dynamic inverse, which well balances the system performance and the tolerance of damage. Firstly, the dynamic model of the aircraft with asymmetric structure damage...
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