The Guidance System of Anti-radiation Aircraft

摘要：

This paper introduced the characteristics ofanti-radiation aircraft and the compositon of itsguidance system.Based on the aerodynamicparameters and actual flight data of a certain type ofairplane,this paper established a mathematical modelof direct lateral force control,and put forward adecoupling method for the system.The systememployer a tracking method in the guidance of theaircraft and gave simulation results.The advantagesof this system are quick response,high percentage ofhits,strong wind-resistance ability and casualty effect.

关键词： anti-radiation aircraft direct lateral force control guidance law tracking method

作者: Taoyun Zhou Yun Cheng Yi Zhang

作者单位: Ddepartment of Communication and Control Engineering,Hunan Institute of Humanities,Science & Technol Ddepartment of Communication and Control Engineering,Hunan Institute of Humanities,Science & Technol School of Electronic Information,Northwestern Polytechnical University,Xian,China

会议类型: 国际会议

会议名称: 2008 3rd International Conference on Intelligent System and Knowledge Engineering(第三届智能系统与知识工程国际会议)(ISKE 2008)

会议地点: 厦门

会议语种:英文

页码: 1352-1356

在线出版日期: 2008-11-17（万方平台首次上网日期，不代表论文的发表时间）