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Chattering-free sliding mode control with unidirectional auxiliary surfaces for miniature helicopters

机译:具有单向辅助表面的小型直升机的无抖动滑模控制

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摘要

Purpose - This article proposes a chattering-free sliding mode control scheme with unidirectional auxiliary surfaces (UAS-SMC) for small miniature autonomous helicopters (Trex 250). Design/methodology/approach - The proposed UAS-SMC scheme consists of a nested sequence of rotor dynamics, angular rate, Euler angle, velocity and position loops. Findings - It is demonstrated that the UAS-SMC strategy can eliminate the chattering phenomenon exhibiting in the convenient SMC method and achieve a better approaching speed. Originality/value - The proposed control strategy is implemented on the helicopter and flight tests clearly demonstrate that a much better performance could be achieved, compared with convenient SMC schemes.
机译:目的-本文提出了一种用于小型自动驾驶直升机(Trex 250)的具有单向辅助表面(UAS-SMC)的无抖动滑模控制方案。设计/方法/方法-提出的UAS-SMC方案由一系列的转子动力学,角速率,欧拉角,速度和位置环组成。结果-证明了UAS-SMC策略可以消除便捷的SMC方法中出现的颤振现象,并达到更快的逼近速度。原创性/价值-拟议的控制策略在直升机上实施,飞行测试清楚地表明,与便捷的SMC方案相比,可以实现更好的性能。

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