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综合火力/飞行控制系统火飞耦合器设计技术研究
引用本文:王新华,杨一栋,周波.综合火力/飞行控制系统火飞耦合器设计技术研究[J].南京航空航天大学学报,2003,35(2):203-207.
作者姓名:王新华  杨一栋  周波
作者单位:1. 南京航空航天大学自动化学院,南京,210016
2. 中国空-空导弹研究院光电部,洛阳,471003
基金项目:航空科学基金 (0 1 E5 2 0 2 8)资助项目
摘    要:为提高武器的攻击精度、延长可攻击时间,本文建议了IFFC系统中的空-空射击作战模态,研究了火飞耦合器的基本结构及其参数优化设计方法,提出了一种以随机射线优化方法和IFFC系统数字仿真相结合的离线寻优的参数设计策略。在寻找过程中采用了以减小脱靶量为优化准则的目标函数。数字仿真表明,优化后的IF-FC系统的可攻击时间延长了30%,攻击精度提高了约50%。本文所提出的设计准则与方法对其它非空-空射击模态的IFFC系统仍有普遍意义。

关 键 词:火飞耦合器  设计  火力控制系统  飞行控制  综合系统
文章编号:1005-2615(2003)02-0203-05
修稿时间:2002年6月6日

Study on Design of Fire/Flight Coupler of Integrated Flight/Fire Control System
Wang Xinhua,Yang Yidong College of Automation Engineering,Nanjing University of Aeronautics & Astronautics,Nanjing,China Zhou Bo.Study on Design of Fire/Flight Coupler of Integrated Flight/Fire Control System[J].Journal of Nanjing University of Aeronautics & Astronautics,2003,35(2):203-207.
Authors:Wang Xinhua  Yang Yidong College of Automation Engineering  Nanjing University of Aeronautics & Astronautics  Nanjing    China Zhou Bo
Institution:Wang Xinhua,Yang Yidong College of Automation Engineering,Nanjing University of Aeronautics & Astronautics,Nanjing,210016,China) Zhou Bo Department of Photoelectricity,Chinese Institute of Air to Air Missile,Luoyang,471003,China
Abstract:In order to improve the attacking accuracy and to prolong the period of exchanging fire, this paper establishes an air to air shooting mode, studies the basic structure and design methods for parameters optimization of fire/flight coupler, and brings forward a design strategy of off line parameter optimization. This strategy combines the optimizing method of random ray and digital simulation of IFFC system. In the course of optimization, an optimizing object function is employed which takes miss distance reducing as the optimizing guideline. Digital simulation results indicate that the period of exchanging fire is prolonged for 30%, and the attacking accuracy is improved for about 50%. The design strategy and guideline can be used in other IFFC systems.
Keywords:integrated flight/fire control  fire/flight coupler  parameter optimization
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