[1]王 杰,丁达理,许 明,等.基于目标机动预估的空空导弹可发射区建模及仿真分析[J].弹道学报,2018,(04):44.[doi:10.12115/j.issn.1004-499X(2018)04-008]
 WANG Jie,DING Dali,XU Ming,et al.Modeling and Simulation Analysis of Allowable Launch Envelopeof Air-to-Air Missile Based on Target Maneuver Estimation[J].Journal Of Ballistics,2018,(04):44.[doi:10.12115/j.issn.1004-499X(2018)04-008]
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基于目标机动预估的空空导弹可发射区建模及仿真分析()
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《弹道学报》[ISSN:1004-499x/CN:32-1343/TJ]

卷:
期数:
2018年04期
页码:
44
栏目:
出版日期:
2018-12-31

文章信息/Info

Title:
Modeling and Simulation Analysis of Allowable Launch Envelopeof Air-to-Air Missile Based on Target Maneuver Estimation
文章编号:
1004-499X(2018)04-0044-09
作者:
王 杰1丁达理1许 明2董康生1库 硕1
1.空军工程大学 航空工程学院,陕西 西安710038; 2.中国人民解放军95478部队,重庆 401329
Author(s):
WANG Jie1DING Dali1XU Ming2DONG Kangsheng1KU Shuo1
1.Aeronautics Engineering College,Air Force Engineering University,Xi’an 710038,China; 2.Unit 95478 of PLA,Chongqing 401329,China
关键词:
空空导弹 可发射区 目标机动预估 改进黄金分割法 不可逃逸区
Keywords:
air-to-air missile allowable launch envelope target maneuver estimation improved golden section method no-escape zone
分类号:
V271.4; TJ765.4
DOI:
10.12115/j.issn.1004-499X(2018)04-008
文献标志码:
A
摘要:
为适应空战中目标逃逸机动的剧烈态势变化,提出了基于目标机动预估的空空导弹可发射区问题,并进行了概念定义; 设计了机动预估模型,根据导弹与目标的相对方位信息,从战术层面对目标逃逸机动方式进行一步预估; 基于多种实际约束,建立了导弹、目标和相对运动模型; 针对黄金分割法在对可发射区解算时存在搜索范围不完备的问题,提出了初始搜索空间自适应动态修正的改进办法; 利用改进的黄金分割搜索策略,实现对可发射区边界值的快速精确搜索。仿真结果表明,基于目标机动预估的可发射区简化了不可逃逸问题的搜索时间,扩大了导弹的攻击范围,有利于导弹战术使用性能的充分发挥。
Abstract:
In order to adapt to the drastic change of target escape maneuver in air combat,the problem of allowable launch envelope of air-to-air missile(AAM)based on target maneuver estimation was presented,and the concept definition of the allowable launch envelope was given. A maneuver prediction model was designed to estimate the one-step target maneuvering from the tactical level. Based on various practical constraints,the missile model,target model and relative motion model were established. The search range is insufficient while the allowable launch envelope is solved by golden section method. Aiming at this problem,an improved method for the adaptive correction of initial search space was proposed. A fast and accurate search of the boundary value of allowable launch envelope was realized by using the improved golden section search strategy. The simulation results show that,the allowable launch envelope based on the target maneuver estimation simplifies the search time of the no-escape problem,and expands the attack range of the missile,and is conducive to the full play of the tactical use performance of missile.

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备注/Memo

备注/Memo:
收稿日期:2018-05-09基金项目:国家自然科学基金项目(61601505); 航空科学基金项目(20155196022)作者简介:王杰(1994- ),男,硕士研究生,研究方向为武器系统与运用工程。E-mail:wangjie_afeu@126.com。
更新日期/Last Update: 2018-12-30