Aircraft modeling method based on variable data length maximum information amount-credibility criterion
A technology with the maximum amount of information and data length, applied in the field of aircraft modeling, it can solve the problems of poor accuracy of aerodynamic model and parameter verification, regardless of data length, etc.
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[0039] The specific steps of the aircraft modeling method based on the variable data length maximum information amount-credibility criterion of the present invention are as follows:
[0040] 1. The commonly used candidate model forms for many aircraft when the angle of attack is less than 60 degrees are:
[0041] x · ( t ) = Φ ( Ω 0 ) f 0 [ x ( t ) ] + θ 1 f 1 [ x ( t ) ] + . . . + θ q f q [ x ...
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