期刊文献+

四旋翼无人机参数预测和抗扰动自适应轨迹跟踪控制

Parameter Prediction and Anti-Disturbance Adaptive Trajectory Tracking Control for UAVs
下载PDF
导出
摘要 为了降低外界环境对四旋翼无人机飞行轨迹的扰动性,提高无人机的控制精度,提出1种基于滑模控制的四旋翼无人机参数预测和抗扰动的自适应轨迹跟踪控制器。这种控制器对四旋翼无人机系统的不确定状态参数、气流、风阻和执行器故障等外界扰动进行预测,实现了对系统输入的状态补偿和扰动补偿,提高了无人机的轨迹跟踪效率和抗扰动能力,消除了机体在飞行过程中的抖振现象,提高了无人机系统对环境的适应性和控制器的稳定性。通过仿真实验,分析了四旋翼无人机在不同控制器作用下的轨迹跟踪性能曲线,验证了所提出的控制器的优越性和有效性。 In order to reduce the disturbance of the external environment on the flight path of a UAV and improve the control accuracy of a UAV,an adaptive trajectory tracking controller based on sliding mode control for a UAV is proposed.This controller can predict the uncertain state parameters, airflow, windage, actuator faults, and other external disturbances of the four rotor UAV system, and realize the state and disturbance compensations of the system input, which can improve trajectory tracking efficiency and anti-interference ability of a UAV,eliminate the body chattering phenomenon in the flight process, and improve the adaptability of UAV system to the environment and the stability of the controller.Through simulation experiments, the trajectory tracking performance curves of four rotor UAV under different controllers are analyzed, and the advantages and effectiveness of the proposed controller are verified.
作者 司勇 王兆魁 李东方 吴奇 SI Yong;WANG Zhao-kui;LI Dong-fang;WU Qi(School of Aerospace Engineering,Tsinghua University,Beijing 100084,China;College of Electrical Engineering and Automation,Fuzhou University,Fuzhou 350108,China;School of Electronic Information and Electrical Engineering,Shanghai Jiao Tong University,Shanghai 200230,China)
出处 《测控技术》 2023年第2期99-107,共9页 Measurement & Control Technology
基金 国家自然科学基金面上项目(62171274)。
关键词 四旋翼无人机 滑模控制 自适应控制 轨迹跟踪 four rotor UAV sliding mode control adaptive control trajectory tracking
  • 相关文献

参考文献2

二级参考文献11

  • 1McKerrow P. Modelling the Draganflyer four-rotor helicopter. Proceedings of the IEEE International Conference on Robotics and Automation. 2004; 3596-3601.
  • 2Pounds P, Mahony R, Hynes P, et al. Design of a four-rotor aerial robot. Proceedings of Australian Conference on Robotics and Automation. 2002; 145-150.
  • 3Tayebi A, McGilvray S. Attitude stabilization of a four-rotor aerial robot. 43rd IEEE Conference on Decision and Control. 2004; 1216-1221.
  • 4Kanellakopoulos I, Krein P. Integral-action nonlinear control of induction motors. Proceedings of the 12th IFAC World Congress. 1993; 251-254.
  • 5Krstic M, Kanellakopoulos I, Kokotovic E Nonlinear and adaptive control design. New York: John Wiley & Sons, 1995.
  • 6Koo T J, Ma Y, Sastry S. Nonlinear control of a helicopter based unmanned aerial vehicle model, http://citeseer.ist.psu.edu/417459.html.
  • 7Prouty R W. Helicopter performance, stability and control. Florida: Krieger Publishing Company, 1996.
  • 8Seddon J. Basic helicopter aerodynamics. Oxford: BSP Professional Books, 1990.
  • 9Smith C, Corripio A. Principles and practice of automatic process control. 2rd ed. New York: John Wiley & Sons, 1997.
  • 10Ashfaq Ahmad Mian.Modeling and Backstepping-based Nonlinear Control Strategy for a 6 DOF Quadrotor Helicopter[J].Chinese Journal of Aeronautics,2008,21(3):261-268. 被引量:54

共引文献62

相关作者

内容加载中请稍等...

相关机构

内容加载中请稍等...

相关主题

内容加载中请稍等...

浏览历史

内容加载中请稍等...
;
使用帮助 返回顶部