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空空拦射导弹火控系统飞行方案建模与仿真
引用本文:袁慧馨.空空拦射导弹火控系统飞行方案建模与仿真[J].飞行力学,2005,23(4):71-73.
作者姓名:袁慧馨
作者单位:中国飞行试验研究院,总工办,陕西,西安,710089
摘    要:针对空空拦射导弹火控系统的飞行试验方案建模与仿真,提出了合理的建模假设,建立了一系列关于载机、目标机及导弹在导弹发射前、发射后整个靶试过程中的运动诸元解算模型,分析了飞机运动方程与火控系统攻击需求之间的相对关系,进行了仿真计算,并将仿真计算结果与实际工程试飞应用结果进行了对比,取到了满意的效果.

关 键 词:空空拦射导弹火控系统  飞行方案  建模与仿真
文章编号:1002-0853(2005)04-0071-03
收稿时间:2005-01-05
修稿时间:2005-09-07

Modelling and Simulation of the Flight Plan for an Air-to-Air Interception Missile Fire Control System
YUAN Hui-xin.Modelling and Simulation of the Flight Plan for an Air-to-Air Interception Missile Fire Control System[J].Flight Dynamics,2005,23(4):71-73.
Authors:YUAN Hui-xin
Abstract:Focusing on the modelling and simulation for an air-to-air interception missile fire control system, this paper puts out a reasonable modelling plan, builds a multi-elements arithmetic model of the movement concerning the carrier, target drones, and the missile before and after its launching, analyes the relative relationship between the kinematic equation of the aircraft and the attack requirements of the fire control system, and carries out the simulation calculations. Furthermore, comparisons between the calculating results of simulations and many successful flight test results have also been made, and the satisfied results have been achieved.
Keywords:air-to-air interception missile fire control system  flight plan  modelling and simulation
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