Aircraft channel coupling coordination control method based on data analysis
A technology of coordinated control and data analysis, applied in the field of flight control, to achieve the effect of coordinated control
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[0052] Now in conjunction with embodiment, accompanying drawing, the present invention will be further described:
[0053] refer to figure 1 , the present invention is a kind of aircraft channel coupling coordination control method based on data analysis, realizes by following steps:
[0054] (a) Using the aircraft re-entry segment dynamics model:
[0055]
[0056] ω=-J -1 ΩJω+J -1 m c (16)
[0057] The dynamic model contains two state variables X=[γ,ω] T and a control input M c ;where, γ=[σ,β,α] T represents the attitude angle vector, σ represents the tilt angle, β represents the sideslip angle, α represents the attack angle, ω=[ω x ,ω y ,ω z ] T Represents the attitude angular rate vector of the aircraft, ω x represents the roll rate, ω y Indicates the yaw rate, ω z Indicates pitch rate, M c =[M x , M y , M z ] T Indicates the control torque of the system, M x Indicates the rolling moment, M y Indicates the yaw moment, M z Indicates the pitching mom...
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