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Nonlinear controller design for a helicopter with an external slung load system

机译:带有外部悬吊负载系统的直升机的非线性控制器设计

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This paper describes a nonlinear deterministic controller design for a helicopter with an underslung external load system. A robust control approach is considered for the control law development. The system is considered as a cascade connection of an uncertain nonlinear system. The controller is designed to ensure the stabilization of the helicopter system and the positioning of the underslung load at hover condition. Control analysis and numerical results show that the proposed controller is able to locate the load at the specified position or its neighbourhood.
机译:本文描述了带有悬空外部负载系统的直升机的非线性确定性控制器设计。在制定控制律时考虑采用鲁棒的控制方法。该系统被视为不确定非线性系统的级联。控制器的设计旨在确保直升机系统的稳定性以及悬停状态下悬吊负载的定位。控制分析和数值结果表明,所提出的控制器能够将负载定位在指定位置或其附近。

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