Design and Simulation of a Kind of Unmanned Helicopter Fixed-Altitude Flight Control System

摘要：

　　In order to improve the stability and the rapidity of Fixed-Altitude unmanned helicopter flight control system,this paper improves the control performance of the closed-loop system by establishing the dynamic mathematical model of unmanned helicopter and adjusts the parameters of the controller under guidance,and completes the simulation with MATLAB.Through the performance evaluation and series,feedback correction,and improved system performance,a quality improvement of unmanned helicopter Fixed-Altitude flight is obtained.This method can reduce the modeling workload and difficulty effectively,and express the process of unmanned helicopter Fixed-Altitude flight intuitively.

关键词： Unmanned helicopter Fixed-Altitude flight Performance evaluation

作者: Wenlai Ma Shouxi Zhu Hongfang Xue

作者单位: Aviation Information Technology R&D Center, Binzhou University, Binzhou, China Department of Computer Science and Technology, Binzhou University, Binzhou, China

会议类型: 国际会议

会议名称: 2013西安国际航空维修与管理学术会议

会议地点: 西安

会议语种:英文

页码: 269-278

在线出版日期: 2013-11-25（万方平台首次上网日期，不代表论文的发表时间）