Hypersonic aircraft self-adaptive learning control method based on deviator characteristic model
An adaptive learning and hypersonic technology, applied in the field of aircraft control, can solve problems such as methods that have no public practical significance
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[0042] The present invention as figure 1 shown in the following steps:
[0043] 1. According to the hypersonic vehicle dynamic equation of the formula group, the offset characteristic model is established.
[0044] Neglecting the effects of the earth's rotation, curvature, and wind, and ignoring the influence of the aerodynamic rudder surface on the aerodynamic force of the aircraft, using the linearized aerodynamic coefficient, the attitude dynamics of the hypersonic aircraft is:
[0045] α · = ω y - ω x cos α tan β - ω z sin α tan β
[0046] β · = ω x sin α - ω z cos α
[0047] ...
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