首页|基于几何控制的四旋翼轨迹跟踪方法

基于几何控制的四旋翼轨迹跟踪方法

扫码查看
针对欠驱动四旋翼无人机在大角度和复杂机动飞行中的控制问题,提出了一种基于几何控制的轨迹跟踪方法,该控制器具有全局稳定性,系统可以从任何初始状态恢复.首先,对四旋翼系统构型进行建模,解决了非线性流形上平移动力学和旋转动力学之间的耦合效应;其次,针对动态系统的基本几何特征,采用微分几何方法设计了跟踪控制器;最后,对该系统进行仿真验证了轨迹跟踪的闭环稳定性.仿真结果表明,当初始姿态误差小于90°时,系统表现出指数稳定性;当初始姿态误差大于90°小于180°时,系统具有全局指数吸引性.
Trajectory Tracking Method of Quadrotor Based on Geometric Control
Aiming at the control problems of under-driven quadrotor UAVs in large-angle and complex maneuvering flight,a trajectory tracking method based on geometric control is proposed.The controller has global stability and the system can recover from any initial state.Firstly,the configuration of the quadrotor system is modeled to solve the coupling effect between translational motion and rotational dynamics on the nonlinear manifold.Secondly,the tracking control is designed by using differential geometry in view of the basic geometric characteristics of the dynamic system.Finally,the system is simulated to verify the closed-loop stabil-ity of trajectory tracking.The simulation results show that when the initial attitude error is less than 90°,the system exhibits expo-nential stability,when the initial attitude error is greater than 90°and less than 180°,the system has global exponential attractive-ness.

quadrotor UAVtrajectory trackingnonlinear manifoldgeometric control

周嘉麒、王指辉、王民泰、印雅萌、翁祥瑞

展开 >

南京航空航天大学 南京 211106

四旋翼 轨迹跟踪 非线性流形 几何控制

南京航空航天大学研究生开放基金项目

kfjj20201506

2024

计算机与数字工程
中国船舶重工集团公司第七0九研究所

计算机与数字工程

CSTPCD
影响因子:0.355
ISSN:1672-9722
年,卷(期):2024.52(4)