现代电子技术Issue(15)：80-83,86,5.
四旋翼无人机设计与滑模控制仿真
Design of quadrotor UAV and its sliding mode control simulation
摘要
Abstract
With the frequent occurrence of natural disasters in recent years,quadrotor UAV search and rescue equipments have been applied widely. The overall design framework of quadrotor aircraft system is introduced. The dynamic model of quadrotor aircraft was established for ground coordinate system and global coordinate system. To obtain fast response speed,and control stability and robustness,sliding mode variable control is used to design aircraft control algorithm. Simulation data are compared between PID controller and the proposed controller,it demonstrates that the strong robustness and control stability of sliding mode variable controller can meet project′s mission requirements.关键词
四旋翼飞行器/滑模变结构控制/PID控制/建模仿真Key words
quadrotor aircraft/sliding mode variable control/PID control/modeling simulation分类
信息技术与安全科学引用本文复制引用
尤元,李闻先..四旋翼无人机设计与滑模控制仿真[J].现代电子技术,2015,(15):80-83,86,5.基金项目
吉林省重点科技攻关项目 （）
