Fuzzy time-delay state feedback control method for uncertain time-delay dual-time-scale systems
A technology of uncertainty and control method, applied in the direction of adaptive control, general control system, control/regulation system, etc., can solve problems such as the inability to eliminate time delay steady-state error
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[0077] Helicopter attitude control system is typical UTDNTTSSs, below the inventive method is applied to the CE150 helicopter attitude control system of Humusoft company, and combines figure 1 and figure 2 , to illustrate its implementation method, the specific process is as follows:
[0078] Step 1: Based on the existing helicopter dynamics model, a continuous-time uncertain time-delay fuzzy singular perturbation model of the helicopter attitude control system is established.
[0079] The schematic diagram of CE150 helicopter attitude control structure is as follows: image 3 As shown, the dynamic model of the helicopter is:
[0080]
[0081] Among them, I d is the moment of inertia of the helicopter along the horizontal axis, T(t) is the driving moment, T f (t) is the friction torque, T m (t) is the gravitational moment, is the attitude angle, and τ is the delay constant.
[0082]
[0083]
[0084] in, is the coefficient of friction, m is the mass of the ...
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