Self-adaptive fault-tolerant control method for hypersonic aircraft
A hypersonic, fault-tolerant control technology, applied in the direction of adaptive control, general control system, control/regulation system, etc., can solve the problem of not considering the influence of disturbance on it
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[0060] The drawings constituting a part of the present invention are used to provide a further understanding of the present invention, and the schematic embodiments and descriptions of the present invention are used to explain the present invention, and do not constitute an improper limitation of the present invention.
[0061] Such as figure 1 As shown, the present embodiment provides an adaptive fault-tolerant control method for a hypersonic vehicle, which specifically includes the following steps:
[0062] (a) Modeling the hypersonic vehicle system, while considering the dynamic impact of modeling uncertainties such as external disturbances on the system;
[0063] (b) Consider H ∞ Performance indicators, establish a robust adaptive observer, obtain the observer design conditions through Lyapunov stability analysis, and ensure that the estimation error of the observer is uniformly bounded under the condition of interference;
[0064] (c) Consider H ∞ Performance indicator...
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