一种直升机非线性轨迹跟踪控制器:设计与实验评估

Gan Yu, Jianan Li, David Cabecinhas, R. Cunha, C. Silvestre
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引用次数: 4

摘要

本文研究了一种能使直升机沿预定轨迹飞行的控制器的设计和实验评估。基于李亚普诺夫方法和反演技术设计了控制器。给出了保证简化直升机模型轨迹跟踪误差收敛于零的推力和角速度控制律。以直升机跟踪椭圆为例,对所提控制器的有效性和性能进行了验证。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
A nonlinear trajectory tracking controller for helicopters: Design and experimental evaluation
This paper addresses the design and experimental evaluation of a controller to steer a helicopter along a desired trajectory. The controller is designed based on Lyapunov's method and backstepping technique. Control laws for thrust and angular velocity are presented that guarantee the convergence of the trajectory tracking error to zero for a simplified helicopter model. Experimental results, which include the helicopter tracking an ellipse, are presented to assess the validity and performance of the proposed controller.
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