TY - JOUR
T1 - 复杂环境对红外空空导弹制导精度影响规律研究
AU - Li, Quancheng
AU - Zhu, Chuanxiang
AU - Fan, Yonghua
AU - Wan, Shizheng
AU - Yan, Jie
N1 - Publisher Copyright:
© 2019 Journal of Northwestern Polytechnical University.
PY - 2019/6/1
Y1 - 2019/6/1
N2 - 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.
AB - 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.
KW - Adjoint analysis model
KW - Barrel roll maneuver
KW - Decoy launch
KW - Guidance accuracy
KW - Infrared guided missile
KW - Miss distance
KW - Strategy
UR - http://www.scopus.com/inward/record.url?scp=85068932058&partnerID=8YFLogxK
U2 - 10.1051/jnwpu/20193730457
DO - 10.1051/jnwpu/20193730457
M3 - 文章
AN - SCOPUS:85068932058
SN - 1000-2758
VL - 37
SP - 457
EP - 464
JO - Xibei Gongye Daxue Xuebao/Journal of Northwestern Polytechnical University
JF - Xibei Gongye Daxue Xuebao/Journal of Northwestern Polytechnical University
IS - 3
ER -