首页 | 本学科首页   官方微博 | 高级检索  
     检索      

建立在视线方程基础上的空战动力学模型
引用本文:宋立国,吴云洁,姜玉宪.建立在视线方程基础上的空战动力学模型[J].北京航空航天大学学报,1999,25(3):306-309.
作者姓名:宋立国  吴云洁  姜玉宪
作者单位:北京航空航天大学,自动控制系
摘    要:首先定义并介绍了视线动力学方程,在此基础上讨论视线坐标系上的机动策略问题。介绍视线坐标系上的空战策略的一种决策方法,以及视线坐标系上的空战策略向机体坐标系上的转化问题。最后建立在机体系上的力和力矩方程,用来说明如何操控飞机达到所需要的空战策略。

关 键 词:动力学方程  机动飞行控制  决策系统  视线动力学方程

Dynamics Model of Air Combat Based on Equations of Line of Sight
Song Liguo,Wu Yunjie,Jiang Yuxian.Dynamics Model of Air Combat Based on Equations of Line of Sight[J].Journal of Beijing University of Aeronautics and Astronautics,1999,25(3):306-309.
Authors:Song Liguo  Wu Yunjie  Jiang Yuxian
Abstract:Dynamics equations of line of sight are defined and introduced in the first. The equations indicates that the accelerations of airplanes have relation with countermeasure state of both sides. Based on this point, maneuver strategies are discussed in the coordinate system of line of sight. A decision method of air combat strategies in the coordinate system of line of sight could be concluded depending on the equation of line of sight angle acceleration. The problem that how to convert the air combat strategies in the coordinate system of line of sight to those in the body reference frame is discussed finally. In order to illustrate how to control airplane to accomplish the needed strategies, equations of force and moment are established.
Keywords:kinetics equations  maneuvering control  decision  making system  dynamics equations of line  of  sight
本文献已被 CNKI 维普 万方数据 等数据库收录!
设为首页 | 免责声明 | 关于勤云 | 加入收藏

Copyright©北京勤云科技发展有限公司  京ICP备09084417号