期刊文献+
共找到2篇文章
< 1 >
每页显示 20 50 100
A Grey Wolf Optimization-Based Tilt Tri-rotor UAV Altitude Control in Transition Mode 被引量:2
1
作者 MA Yan WANG Yingxun +2 位作者 CAI Zhihao ZHAO Jiang LIU Ningjun 《Transactions of Nanjing University of Aeronautics and Astronautics》 EI CSCD 2022年第2期186-200,共15页
To solve the problem of altitude control of a tilt tri-rotor unmanned aerial vehicle(UAV)in the transition mode,this study presents a grey wolf optimization(GWO)based neural network adaptive control scheme for a tilt ... To solve the problem of altitude control of a tilt tri-rotor unmanned aerial vehicle(UAV)in the transition mode,this study presents a grey wolf optimization(GWO)based neural network adaptive control scheme for a tilt trirotor UAV in the transition mode.Firstly,the nonlinear model of the tilt tri-rotor UAV is established.Secondly,the tilt tri-rotor UAV altitude controller and attitude controller are designed by a neural network adaptive control method,and the GWO algorithm is adopted to optimize the parameters of the neural network and the controllers.Thirdly,two altitude control strategies are designed in the transition mode.Finally,comparative simulations are carried out to demonstrate the effectiveness and robustness of the proposed control scheme. 展开更多
关键词 tilt tri-rotor unmanned aerial vehicle altitude control neural network adaptive control grey wolf optimization(GWO)
下载PDF
Sliding Mode Control-Based Autonomous Control of a Tri-rotor Unmanned Aerial Vehicle
2
作者 Abid Raza Fahad Mumtaz Malik +3 位作者 Rameez Khan Naveed Mazhar Hameed Ullah Nigar Ahmed 《Guidance, Navigation and Control》 2021年第3期52-75,共24页
A nonlinear control technique for autonomous control of a tri-rotor unmanned aerial vehicle is presented in this paper.First,a comprehensive mathematical model is developed using the Newton–Euler approach for a tri-r... A nonlinear control technique for autonomous control of a tri-rotor unmanned aerial vehicle is presented in this paper.First,a comprehensive mathematical model is developed using the Newton–Euler approach for a tri-rotor,which is found to be highly nonlinear and coupled.Then,the equivalent input a±ne model is extracted by applying a suitable transformation.Finally,the sliding mode control for trajectory tracking is chosen which is immune to matched external disturbances,parametric uncertainties,and modeling errors.The proposed controller performance has been veri¯ed for appropriate inputs under wind disturbances using MATLAB,and the simulation results are presented. 展开更多
关键词 Autonomous control nonlinear control sliding mode control unmanned aerial vehicle tri-rotor
原文传递
上一页 1 下一页 到第
使用帮助 返回顶部