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Adaptive backstepping trajectory tracking controller for a miniature helicopter

机译:小型直升机的自适应反步轨迹跟踪控制器

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An adaptive backstepping controller is proposed to achieve the asymptotically stable trajectory tracking for a miniature helicopter. The helicopter model is firstly decomposed into a cascaded structure between the position and attitude loops with unmodeled dynamics. The backstepping technique is applied to exploit this cascaded structure and to streamline the controller design procedure. Hyperbolic tangent functions, instead of traditional sign functions, are adopted to complete adaptive algorithms for adjusting the upper bounds of the unmodeled dynamics. Further, the controller introduces an auxiliary dynamic system to ensure the thrust constraint and to obviate singularity during the command attitude extraction. The stability analysis demonstrates that, the asymptotical stability of the auxiliary dynamic system warrants the asymptotically stable tracking of the miniature helicopter system. Simulations verify the theoretical results and analyze the tracking performance. Copyright (c) 2016 John Wiley & Sons, Ltd.
机译:提出了一种自适应反推控制器来实现微型直升机的渐近稳定轨迹跟踪。首先将直升机模型分解为位置和姿态环之间的级联结构,并具有未建模的动力学。应用反推技术来开发这种级联结构并简化控制器设计过程。采用双曲正切函数代替传统符号函数来完成自适应算法,以调整未建模动力学的上限。此外,控制器引入了辅助动力系统,以确保推力约束并避免在命令姿态提取过程中出现奇点。稳定性分析表明,辅助动力系统的渐近稳定性保证了微型直升机系统的渐近稳定跟踪。仿真验证了理论结果并分析了跟踪性能。版权所有(c)2016 John Wiley&Sons,Ltd.

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