首页> 外文期刊>Mechanical systems and signal processing >Asymptotic tracking control of an underactuated tilt trirotor unmanned aerial vehicle
【24h】

Asymptotic tracking control of an underactuated tilt trirotor unmanned aerial vehicle

机译:疏水倾斜三风无人空中车辆的渐近跟踪控制

获取原文
获取原文并翻译 | 示例
           

摘要

In this paper, a novel nonlinear tracking control strategy is developed for an underactuated tilt trirotor unmanned aerial vehicle (UAV) which is subject to unknown external disturbances. The control scheme is developed based on the inner-loop-outer-loop methodology. Both effects of the unknown external disturbances on the inner-loop and outer-loop are compensated through the proposed control law. The unknown external disturbances which affect the outer-loop (or position loop) are compensated via a nonlinear observer that is designed based on the super-twisting method. The unknown external disturbances that affect the inner-loop (or attitude loop) are rejected via a sliding-mode based nonlinear robust control component. The stability of the closed-loop system for the tilt trirotor UAV, together with the convergence of the UAV's position and heading tracking errors, are proved via a Lyapunov based stability analysis. Hardware-in-loop (HIL) flight experiments are performed to validate the control performance of the proposed nonlinear robust control strategy.
机译:在本文中,开发了一种新的非线性跟踪控制策略,用于欠型倾斜三通型空中航空车(UAV),其受到未知的外部干扰。基于内环外回路方法开发控制方案。通过所提出的控制法律补偿未知的外部干扰对内环和外环的两种效果。影响外环(或位置环)的未知外部干扰通过基于超捻方法设计的非线性观察者来补偿。通过基于滑模的非线性鲁棒控制组件拒绝影响内圈(或姿态环路)的未知外部干扰。通过基于Lyapunov的稳定性分析证明,通过基于Lyapunov的稳定性分析证明了倾斜Trivoror UAV的闭环系统的稳定性以及UAV位置和前置跟踪误差的收敛。进行硬件循环(HIL)飞行实验,以验证所提出的非线性鲁棒控制策略的控制性能。

著录项

相似文献

  • 外文文献
  • 中文文献
  • 专利
获取原文

客服邮箱:kefu@zhangqiaokeyan.com

京公网安备:11010802029741号 ICP备案号:京ICP备15016152号-6 六维联合信息科技 (北京) 有限公司©版权所有
  • 客服微信

  • 服务号