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Adaptive control system for autonomous helicopter slung load operations

机译:自主直升机直升式装载作业的自适应控制系统

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This paper presents design and verification of an estimation and control system for a helicopter slung load system. The estimator provides position and velocity estimates of the slung load and is designed to augment existing navigation in autonomous helicopters. Sensor input is provided by a vision system on the helicopter that measures the position of the slung load. The controller is a combined feedforward and feedback scheme for simultaneous avoidance of swing excitation and active swing damping. Simulations and laboratory flight tests show the effectiveness of the combined control system, yielding significant load swing reduction compared to the baseline controller.
机译:本文介绍了直升机悬挂负载系统的估计和控制系统的设计和验证。估计器提供了斜摆负载的位置和速度估计,旨在增强自动直升机的现有导航能力。传感器输入由直升机上的视觉系统提供,该视觉系统可测量倾斜负载的位置。该控制器是前馈和反馈的组合方案,可同时避免摆动激励和主动摆动阻尼。仿真和实验室飞行测试证明了组合控制系统的有效性,与基线控制器相比,可显着降低负载摆动。

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