四旋翼飞行器鲁棒自适应姿态控制器设计
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Design of Robust Adaptive Attitude Controller for Quadrotor
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    摘要:

    为实现四旋翼飞行器姿态的稳定控制,针对该系统的非线性、易受外界干扰和参数摄动影响等问题,提 出一种鲁棒自适应控制方法。首先通过分析四旋翼飞行器的工作原理,建立了动力学模型;其次在线性化飞行器模 型的基础上,设计了基于最优二次型鲁棒伺服控制方法的姿态控制器;然后应用模型参考自适应控制方法设计了自 适应补偿器消除系统不确定性的影响;最后对加入了鲁棒自适应控制的飞行器进行仿真。仿真结果表明:该控制器 具有稳定精确的指令跟踪性能和强鲁棒性,能够在复杂环境下实现稳定良好的姿态控制。

    Abstract:

    In order to realize stable attitude control of the quadrotor, a robust adaptive control method was proposed to solve the problems of nonlinearity and being easily influenced by the external environment. First of all, the dynamic model was established by analyzing the working principle of the quadrotor. Besides, upon the linear model, attitude controllers were designed based on optimal robustness servo control method. Additionally, model reference adaptive control method was applied to design the adaptive compensator for eliminating the influence of system uncertainty. Finally, the simulation results were presented to prove that robust adaptive controllers achieved stable control in complex environment and had accurate command tracking performance and strong robustness.

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引用本文

堵湘君.四旋翼飞行器鲁棒自适应姿态控制器设计[J].,2018,37(08).

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历史
  • 收稿日期:2018-03-24
  • 最后修改日期:2018-04-29
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  • 在线发布日期: 2018-09-18
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