An online identification method of aircraft aerodynamic characteristics based on backtracking adaptive algorithm
A technology of aerodynamic characteristics and identification methods, applied in the field of online identification of aircraft aerodynamic characteristics, can solve the problems of inability to adapt to the online rapid identification of near-space aircraft, the difficulty of online identification, and the large amount of calculation
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[0066] The present invention will be analyzed in detail below in conjunction with the accompanying drawings and specific embodiments.
[0067] Taking the relatively complex lateral and lateral aerodynamic characteristics identification method as an example, theoretical analysis is carried out (the identification of longitudinal aerodynamic characteristics can be compared):
[0068] 1. Mathematical problem description and problem conversion
[0069] Consider the following dynamic equations for the lateral and lateral attitude of a plane-symmetric aircraft:
[0070]
[0071] In the formula, ω x is the roll angular velocity, ω y is the yaw rate, ω z is the pitch angular velocity, J x is the moment of inertia of the aircraft around the roll axis, J y is the moment of inertia of the aircraft around the yaw axis, J z is the moment of inertia of the aircraft around the pitch axis, J xy is the inertia product of the aircraft about the yaw axis y and the roll axis x.
[0072...
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