Evaluation and Enhancing Missile performance via Real Time Flight Simulation Model

摘要：

　　Simulation is a very important tool of design and development of systems; especially in the field of guidance and control.This paper discusses first,the implementation and evaluation of a real time Six Degree Of Freedom(6DOF)flight simulation model for a Skid-To-Turn(STT)Infra Red(IR)rolling missile with a single plane of control.Second,applying True Proportional Navigation(TPN)instead of Classical Proportional Navigation(CPN)guidance law that is used in guidance system of real missile.As a result of applying TPN guidance law,the autopilot gain in the flight control system is recalculated to enhance missile performance.Simulation results when using TPN guidance law are evaluated and compared with simulation results when using CPN guidance law.The comparison results prove that TPN increases the ability of missile to hit more speed and maneuvering targets.

关键词： Homing Guidance Systems 6DOF Flight Simulation Model Rolling Missile with Single Plane of Control

作者: Ahmed AWAD Haoping WANG

作者单位: Sino-French International Joint Laboratory of Automatic Control and Signal Processing(LaFCAS),Automation School,Nanjing University of Science & Technology,Nanjing 210094,China

会议类型: 国际会议

会议名称: The 33th Chinese Control Conference第33届中国控制会议

会议地点: 南京

会议语种:英文

页码: 6324-6329

在线出版日期: 2014-07-28（万方平台首次上网日期，不代表论文的发表时间）