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首页> 外文期刊>International journal of systems science >Robust output tracking control of a laboratory helicopter for automatic landing
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Robust output tracking control of a laboratory helicopter for automatic landing

机译:用于自动降落的实验室直升机的鲁棒输出跟踪控制

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摘要

In this paper, robust output tracking control problem of a laboratory helicopter for automatic landing in high seas is investigated. The motion of the helicopter is required to synchronise with that of an oscillating platform, e.g. the deck of a vessel subject to wave-induced motions. A robust linear time-invariant output feedback controller consisting of a nominal controller and a robust compensator is designed. The robust compensator is introduced to restrain the influences of parametric uncertainties, nonlinearities and external disturbances. It is shown that robust stability and robust tracking property can be achieved simultaneously. Experimental results on the laboratory helicopter for automatic landing demonstrate the effectiveness of the designed control approach.
机译:本文研究了公海自动降落的实验室直升机的鲁棒输出跟踪控制问题。要求直升机的运动与摆动平台的运动同步,例如受波浪引起的运动的船舶甲板。设计了一种由标称控制器和鲁棒补偿器组成的鲁棒线性时不变输出反馈控制器。引入了鲁棒补偿器,以抑制参数不确定性,非线性和外部干扰的影响。结果表明,可以同时实现鲁棒的稳定性和鲁棒的跟踪特性。在用于自动降落的实验室直升机上的实验结果证明了所设计的控制方法的有效性。

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