Self-adaption low-order controller for unmanned helicopter
A technology for unmanned helicopters and controllers, applied in adaptive control, general control systems, control/regulation systems, etc., can solve problems such as numerical instability, achieve stable control, and facilitate the handling of control constraints and state constraints
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[0035] The present invention will be further described in detail below in conjunction with the accompanying drawings and embodiments.
[0036] The order of the control object is high (infinite in theory), but the controller design can only be of low order. The controlled object has parameter uncertainty and disturbance uncertainty. The basic form of the controller is (taking PD as an example):
[0037] τ 2 (s) = τ 21 (s)+τ 22 (s)+τ 23 (s)
[0038] In the formula, τ 21 (s)=-(k p +k d s) θ(s),
[0039]
[0040]
[0041] Among them, τ 2 (s) represents the control quantity of the controlled system; τ 21 (s), τ 22 (s), τ 23 (s) represents the control component of the controlled system; k p 、k d 、k i 、k in 、k f represents the controller parameters; θ(t) represents the pitch angle; ω d , ω z , ω f Represents the closed-loop system bandwidth; ξ z , ξ f represents the system damping. Control component τ 21 (s) has a PD control form, which is used to incre...
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