Variant aircraft control method based on composite intelligent learning
A technology of variant aircraft and control method, applied in the field of aircraft control, can solve problems such as the inability to approach unknown dynamics and the inability to achieve precise tracking of the system
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[0089] Now in conjunction with embodiment, accompanying drawing, the present invention will be further described:
[0090] refer to figure 1 , the present invention is based on the variant aircraft control method of composite intelligence learning and is applied to the variable-sweep wing aircraft, and is realized through the following steps:
[0091] (a) Considering the longitudinal dynamics model of the variable-sweep wing aircraft
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[0097] Among them, F Ix , F Ikz , F Iz and M Iy Indicates the moment of inertia caused by the deformation process, and its expression is
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[0099] The dynamic model contains five state variables X=[V, h, γ, α, q] T and two control inputs U=[δ e ,T] T , where V represents velocity, h represents height, γ represents track angle, α represents angle of attack, q represents pitch angle velocity, δ e Indicates rudder deflection angle, T indicates thrust; D, L and M A resp...
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