Hypersonic aircraft high-safety anti-interference control method by considering attack angle limitation
A control method and hypersonic technology, applied in vehicle position/route/altitude control, attitude control, control/regulation system, etc., can solve the problem of inability to guarantee the angle of attack constraint a priori, relying on high-level full state measurement, etc., to achieve strong attack Corner safety constraint characteristics, the effect of achieving precise tracking control, and low online computational complexity
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[0036] The present invention will be further described below in conjunction with specific examples.
[0037] A high-safety anti-interference control method for a hypersonic vehicle considering a limited angle of attack, comprising the following steps:
[0038] (1) Establish AHV longitudinal motion / dynamic model including external disturbance:
[0039]
[0040] Among them, V is velocity, h is altitude, γ is track inclination, α is angle of attack, Q is pitch angle velocity, Φ is throttle opening, δ e is the rudder deflection angle, f j and g j (j=V, γ, α, Q) denote the aggregate disturbance and AHV nominal dynamics, respectively, defined as follows:
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[0044]
[0045] Among them, m=300 and I yy =86722.54 represents the mass and moment of inertia of the aircraft respectively, g=1.41×10 16 represents the gravitational constant, Δ represents the perturbation of the aerodynamic coefficient, d ve = 1 means the external disturbance of the ...
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