| 综合火力/飞行控制系统轰炸模态的设计 |
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| 引用本文： | 王庆田,杨一栋,王新华,周波,邹庆元.综合火力/飞行控制系统轰炸模态的设计[J].海军航空工程学院学报,2004,19(5):513-516. |
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| 作者姓名： | 王庆田 杨一栋 王新华 周波 邹庆元 |
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| 作者单位： | 1. 南京航空航天大学自动化学院,南京,210016
2. 中航一集团613研究所,洛阳,471003 |
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| 基金项目： | 国防基础研究基金项目资助(编号:K1603060319) |
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| 摘 要： | 在无人驾驶状态下,对大机动转弯状态下空地轰炸模态的基本框架的实现技术进行了研究,导出了该模态的综合火力/飞行系统的火控解算方程,提出了火/飞耦合器的设计方法,并对飞控系统进行了设计,最终给出的无人驾驶机动轰炸模态综合火力/飞行系统数字仿真验证表明提出的设计技术是可行的,明显地提高了攻击精度。
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| 关 键 词： | 轰炸模态 综合火力/飞行控制 火/飞耦合器 |
| 修稿时间： | 2003年10月6日 |
Design of Bombing Model for Integrated Flight And Fire Control System |
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| WANG Qing-tian,YANG Yi-dong,WANG Xin-hua,ZHOU Bo,ZOU Qing-yuan.Design of Bombing Model for Integrated Flight And Fire Control System[J].Journal of Naval Aeronautical Engineering Institute,2004,19(5):513-516. |
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| Authors: | WANG Qing-tian YANG Yi-dong WANG Xin-hua ZHOU Bo ZOU Qing-yuan |
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| Institution: | WANG Qing-tian YANG Yi-dong WANG Xin-hua College of Automation Engineering,Nanjing University of Aeronautics & Astronautics,Naujing,210016,ZHOU Bo ZOU Qing-yuan No.613 Institute of Chinese First Aeronautical Group,Luoyang,471003 |
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| Abstract: | In order to improve the viability of unmanned attacker in auto-bombing mode at low altitude,the paper brings forward a main frame of the air-to-ground bombing mode in a state of abrupt turn.This paper studies the realization of this mode when used in unmanned attacker,deduces the calculation equation of fire control in integrated flight/fire control system,advances the design method of fire/flight coupler,and designs the flight control system.At the end,this paper presents the digital simulation results of the whole system,which indicate that the design method of this paper is feasible,and obviously improving the precision of attacking. |
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| Keywords: | bombing model integrated flight and fire control flight and fire coupler |
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