Hypersonic aircraft elevator fault control method
A hypersonic, aircraft technology, applied in the direction of adaptive control, general control system, control/regulation system, etc., can solve the problems of aircraft influence, complex flight dynamics characteristics of hypersonic aircraft, large uncertainty, etc.
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[0073] Below in conjunction with accompanying drawing, a kind of hypersonic vehicle elevator failure control method proposed by the present invention is described in detail:
[0074] The present invention provides a kind of hypersonic vehicle elevator failure control method, comprising the following steps:
[0075] Step 1, establish the longitudinal kinematics and dynamics model of the cruise segment of the hypersonic vehicle, the model is expressed as:
[0076] V · = T cos α - D m - μ sin γ r 2
[0077] γ · = L + T sin α mV - ...
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