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论文:2019,Vol:37,Issue(3):457-464 |
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引用本文： |
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李权成, 朱传祥, 凡永华, 万士正, 闫杰. 复杂环境对红外空空导弹制导精度影响规律研究[J]. 西北工业大学学报 |
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LI Quancheng, ZHU Chuanxiang, FAN Yonghua, WAN Shizheng, YAN Jie. Study on Infrared Air-to-Air Missile Guidance Accuracy Affected by Complicated Environment[J]. Northwestern polytechnical university |
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| 复杂环境对红外空空导弹制导精度影响规律研究 |
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| 李权成1, 朱传祥2, 凡永华1, 万士正1, 闫杰1 |
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1. 西北工业大学 航天学院, 陕西 西安 710072;
2. 西北工业大学 机电学院, 陕西 西安 710072 |
| 摘要: |
| 红外空空导弹制导精度受目标机动、干扰以及自然环境等多种因素影响。考虑目标机动和投放诱饵弹所构成的复杂对抗环境，通过分析点源诱饵弹干扰过程、运动特性以及对制导系统的作用机理，建立了更符合实际情况的目标机动和诱饵投放对导弹制导精度影响的伴随分析模型。利用伴随法，分析了目标机桶滚角速率以及诱饵弹的齐投数量、起燃时间、投放间隔与策略对导弹脱靶量的影响规律，为战斗机采取对抗红外空空导弹策略提供参考。 |
| 关键词:
桶滚机动
诱饵投放
策略
红外制导导弹
制导精度
脱靶量
伴随分析模型
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| Study on Infrared Air-to-Air Missile Guidance Accuracy Affected by Complicated Environment |
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| LI Quancheng1, ZHU Chuanxiang2, FAN Yonghua1, WAN Shizheng1, YAN Jie1 |
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1. School of Astronautics, Northwestern Polytechnical University, Xi'an 710072, China;
2. School of Mechanical Engineering, Northwestern Polytechnical University, Xi'an 710072, China |
| Abstract: |
| The guidance accuracy of an infrared air-to-air missile is affected by various factors such as target maneuver, interference, and the natural environment. The complicated confrontational environment posed by target maneuver and decoy launch is considered in this article. The more practical adjoint analysis model for the influence of target maneuver and decoy launch on missile guidance accuracy is established by analyzing the jamming process, motion characteristics, and the influence mechanism on the guidance system of point source decoy. By using the adjoint method, the barrel roll maneuver angular rate, the numble of simultaneous decoy launch, the ignition time, the interval between launches and the strategy influence on the miss distance of the missile are analyzed in detail, which will provide strategic references for the aircraft to fight against the infrared air-to-air missiles. |
| Key words:
barrel roll maneuver
decoy launch
strategy
infrared guided missile
guidance accuracy
miss distance
adjoint analysis model
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| 收稿日期: 2018-05-27
修回日期:
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| DOI: 10.1051/jnwpu/20193730457 |
| 通讯作者:
Email： |
| 作者简介: 李权成(1989-),西北工业大学博士研究生,主要从事飞行器制导与控制研究。
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