小型无人直升机非线性控制设计与稳定性分析

Lin Zhang, Z. Ding
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引用次数: 4

摘要

本文主要研究了微型无人直升机的非线性控制器设计和稳定性分析。我们的工作是利用非线性控制方法来控制无人直升机的动力学,将其分为较慢的平移动力学(外环)和较快的方向动力学(内环),从而表现出分层结构。分别属于内环和外环的姿态角和位置可以采用后退控制策略进行独立控制。在设计控制器后,对直升机系统进行了包括扑翼动力学在内的稳定性分析。
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Nonlinear control design and stability analysis of a small-scale unmanned helicopter
The main focus of this paper is to design nonlinear controllers and analyse stability for a miniature unmanned helicopter. Our work is to utilize nonlinear control methodology to command dynamics of unmanned helicopter which has been divided into slower translational dynamics (outer-loop) and faster orientation dynamics (inner-loop), thus exhibiting hierarchical structure. The attitude angles and position which separately belong to the inner-loop and the outer-loop can be independently controlled by backstepping control strategy. Stability analysis of the helicopter system including flapping dynamics has been presented after designing controllers.
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