@inproceedings{e1e71bef48c24a9db12adbc527bb18a6,
title = "An Impact Angle Control Guidance via Self-restrained Look Angle Shaping",
abstract = "An impact angle control guidance called IACG is proposed by shaping the look angle as a function of missile-target distance. The proposed guidance law is proved to be a kind of proportional navigation guidance with a time-dependent guidance coefficient, where only the line-of-sight rate and look angle are required. The derivation of IACG does not involve linearization as well as estimation of time-to-go, thus can ensure the accuracy of the guidance result. Further, the look angle can realize self-restrained due to the tangent function in the shaping without any other special design on the look angle. The effects of parameter values on the performance of IACG are also discussed. Nonlinear numerical simulations are carried out to confirm the effectiveness and stability of the guidance law.",
keywords = "Impact angle, Look angle self-restrained, Look angle shaping",
author = "Xiangxiang Li and Wanchun Chen and Zhongyuan Chen and Shen Zhang",
note = "Publisher Copyright: {\textcopyright} 2023, The Author(s), under exclusive license to Springer Nature Singapore Pte Ltd.; International Conference on Guidance, Navigation and Control, ICGNC 2022 ; Conference date: 05-08-2022 Through 07-08-2022",
year = "2023",
doi = "10.1007/978-981-19-6613-2\_583",
language = "英语",
isbn = "9789811966125",
series = "Lecture Notes in Electrical Engineering",
publisher = "Springer Science and Business Media Deutschland GmbH",
pages = "6033--6042",
editor = "Liang Yan and Haibin Duan and Yimin Deng and Liang Yan",
booktitle = "Advances in Guidance, Navigation and Control - Proceedings of 2022 International Conference on Guidance, Navigation and Control",
address = "德国",
}