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Spot hover control of helicopter and swing control of helicopter sling load by using Zhang-gradient method

机译:张梯度法控制直升机的悬停控制和吊索载荷的摆动控制

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摘要

Helicopter sling load has a wide range of applications. However, the sling load of helicopter may make it dangerous. In this paper, the spot hover control and the swing control of helicopter sling load system are investigated. To solve the problems, the ZG method, which is the combination of Zhang dynamics (ZD) and gradient dynamics (GD) methods, is adopted. Firstly, with the purpose of helicopter spot hover considered, a z2g1 controller is designed and proposed by using the ZG method, where ZD is used for two times and GD is used for one time. Secondly, with the purpose of swing control of helicopter sling load considered, another z2g1 controller is designed and proposed. Simulation results on a mathematical model of helicopter sling load system equipped with the proposed z2g1 controllers are presented for different control purposes, which substantiate the effectiveness and significance of the proposed method and controllers.
机译:直升机吊索负载具有广泛的应用范围。但是,直升飞机的吊索可能会造成危险。本文研究了直升机悬带载荷系统的悬停控制和摆动控制。为了解决这些问题,采用了ZG方法,即Zhang动力学(ZD)和梯度动力学(GD)方法的组合。首先,考虑到直升机的悬停目的,采用ZG方法设计并提出了一种z2g1控制器,其中ZD使用两次,GD使用一次。其次,针对直升机吊索载荷的摆动控制,设计并提出了另一种z2g1控制器。针对不同的控制目的,提出了装备有所提出的z2g1控制器的直升机悬索负载系统的数学模型的仿真结果,证实了所提出的方法和控制器的有效性和重要性。

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