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Quadcopter formation flight control combining MPC and robust feedback linearization

机译:结合MPC和强大反馈线性化的四旋翼编队飞行控制

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摘要

This paper presents an integrated and practical control strategy to solve the leader-follower quadcopter formation flight control problem. To be specific, this control strategy is designed for the follower quadcopter to keep the specified formation shape and avoid the obstacles during flight. The proposed control scheme uses a hierarchical approach consisting of model predictive controller (MPC) in the upper layer with a robust feedback linearization controller in the bottom layer. The MPC controller generates the optimized collision-free state reference trajectory which satisfies all relevant constraints and robust to the input disturbances, while the robust feedback linearization controller tracks the optimal state reference and suppresses any tracking errors during the MPC update interval. In the top-layer MPC, two modifications, i.e. the control input hold and variable prediction horizon, are made and combined to allow for the practical online formation flight implementation. Furthermore, the existing MPC obstacle avoidance scheme has been extended to account for small non-apriorily known obstacles. The whole system is proved to be stable, computationally feasible and able to reach the desired formation configuration in finite time. Formation flight experiments are set up in Vicon motion-capture environment and the flight results demonstrate the effectiveness of the proposed formation flight architecture.
机译:本文提出了一种综合而实用的控制策略,以解决跟随跟随者的四旋翼编队的飞行控制问题。具体来说,该控制策略是为随动四轴飞行器设计的,以保持指定的编队形状并避免飞行中的障碍物。所提出的控制方案使用一种分层方法,该方法由上层的模型预测控制器(MPC)和底层的鲁棒反馈线性化控制器组成。 MPC控制器生成优化的无冲突状态参考轨迹,该轨迹满足所有相关约束并且对输入干扰具有鲁棒性,而鲁棒的反馈线性化控制器跟踪最佳状态参考并抑制MPC更新间隔期间的任何跟踪误差。在顶层MPC中,进行了两种修改,即控制输入保持和可变预测范围,并进行了组合,以实现实际的在线编队飞行实施。此外,现有的MPC避障方案已扩展为解决小的非先验已知障碍。事实证明,整个系统是稳定的,计算上可行的,并且能够在有限的时间内达到所需的地层构造。在Vicon运动捕捉环境中进行了编队飞行实验,飞行结果证明了所提出的编队飞行架构的有效性。

著录项

  • 来源
    《Journal of the Franklin Institute》 |2014年第3期|1335-1355|共21页
  • 作者

    Weihua Zhao; Tiauw Hiong Go;

  • 作者单位

    School of Mechanical and Aerospace Engineering, Nanyang Technological University, Singapore 639798, Singapore;

    Mechanical and Aerospace Engineering Department, Florida Institute of Technology, Melbourne, FL 32901, USA;

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  • 正文语种 eng
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