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Singularity-free non-linear controller for a model-scaled autonomous helicopter

机译:模型规模自动直升机的无奇异非线性控制器

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摘要

A singularity-free non-linear controller is proposed for trajectory tracking of a model-scaled autonomous helicopter. The helicopter model is firstly decomposed into a nominal one with unmodelled dynamics. Based on the decomposed model, the controller is designed with the hierarchical inner-outer loop strategy. The outer position loop controller is designed with hyperbolic tangent functions, and criteria for controller parameter selections are developed to realise the position tracking and to obviate singularity in deriving the command attitude from the position loop controller. The inner attitude loop controller is designed based on barrier Lyapunov function and backstepping technique to achieve the attitude tracking without singularity during the tracking process. In addition, in order to improve the tracking performance, observers are employed to compensate the unmodelled dynamics. Simulation of two manoeuvres verify the proposed theoretical results.
机译:提出了一种无奇异的非线性控制器,用于模型规模自主直升机的轨迹跟踪。首先将直升机模型分解为具有未建模动力学的名义模型。在分解模型的基础上,采用分层内外环策略设计控制器。外部位置环控制器设计有双曲正切函数,并开发了用于控制器参数选择的标准,以实现位置跟踪并消除从位置环控制器得出命令姿态时的奇异性。基于障碍Lyapunov函数和后推技术设计了内部姿态环控制器,以在跟踪过程中实现无奇异的姿态跟踪。另外,为了提高跟踪性能,采用观察者来补偿未建模的动力学。两次演算的仿真验证了所提出的理论结果。

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  • 来源
    《Control Theory & Applications, IET》 |2016年第2期|210-219|共10页
  • 作者

    Yao Zou; Wei Huo;

  • 作者单位

    Sci. & Technol. on Aircraft Control Lab., Beihang Univ., Beijing, China;

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  • 原文格式 PDF
  • 正文语种 eng
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