Aircraft modeling method based on variable measurement number maximum information criterion
A technology with the largest amount of information and modeling method, applied in the field of aircraft modeling, it can solve problems such as poor accuracy of aerodynamic model and parameter verification
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[0046] The specific steps of the aircraft modeling method based on the variable measurement number maximum information amount criterion of the present invention are as follows:
[0047] 1. The commonly used candidate model forms for many aircraft when the angle of attack is less than 60 degrees are:
[0048] x · ( t ) = Φ ( Ω 0 ) f 0 [ x ( t ) ] + θ 1 f 1 [ x ( t ) ] + . . . ...
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