We mainly studied the design of three attitudes controller and the anti-windup control for helicopter with actuators saturation in this paper.
最后，本文对直升机的执行器饱和问题进行了抗饱和控制器设计方法的研究。
In order to prevent the problems by using classical Anti-windup (AW), the state tracking AW design is presented.
针对传统的AW设计的问题，该文采用基于状态跟踪的AW设计方法。
In order to prevent the problems by using classical Anti-windup (AW), the state tracking AW design is presented.
针对传统的AW设计的问题，该文采用基于状态跟踪的AW设计方法。
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