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无人动力伞飞行航路自主控制方法研究
引用本文:张晨,李小民. 无人动力伞飞行航路自主控制方法研究[J]. 计算机测量与控制, 2010, 18(4)
作者姓名:张晨  李小民
作者单位:军械工程学院,光学与电子工程系,河北,石家庄,050003
摘    要:根据无人动力伞的特点,提出了一种无人动力伞飞行航路自主控制方法;研究了动力伞的自主导航原理,重点分析了动力伞航路预置的方法,并给出了航线的设定与规划,同时给出了根据GPS反馈的飞行实时状态对航路进行检测的具体方法;并在自行开发的动力伞航路自主控制演示平台上,对动力伞自主飞行控制系统进行仿真;试验证明,无人动力伞基本能按照预定航线进行自主飞行,系统有较好的动态特性和稳态控制精度,达到了预期的目标。

关 键 词:动力伞  自主导航  航迹控制  

Research on Autonomous Flight Track Control Method of Unmanned Powered Parachute
Zhang Chen,Li Xiaomin. Research on Autonomous Flight Track Control Method of Unmanned Powered Parachute[J]. Computer Measurement & Control, 2010, 18(4)
Authors:Zhang Chen  Li Xiaomin
Affiliation:Optics and Electron Engineering Department College of Ordnance Engineering/a>;Shijiazhuang 050003/a>;China
Abstract:According to the characteristics of unmanned Powered Parachute,an unmanned autonomous flight route control methods is proposed.Studied the Powered Parachute's autonomous navigation principles,focused on analyzing the method of pre-setting of Powered Parachute route,and gives the concrete methods of the setting and planning routes,and gives feedback based on GPS real-time status of the route of flight testing.Test proved that the system has good dynamic performance and steady-state control accuracy to achiev...
Keywords:powered parachute  autonomous navigation  aircraft control  
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