@inproceedings{4b1135f7366d446086c1579034b670aa,
title = "Integrated Guidance and Control Design for Homing Missile with Terminal Angular Constraint",
abstract = "Aiming at homing missiles, an integrated guidance and control (IGC) design scheme is developed. Meanwhile, the situation of terminal angular constraint is also taken into account. Firstly, considering a kind of homing missile, the nonlinear mathematical model is formulated in the longitudinal plane. For the purpose of dealing with the numerous states regulation problem of such a nonlinear system, a novel dynamic surface control algorithm combined with adaptive control law is deduced based on the backstepping approach. It is testified that the developed control scheme is capable of simultaneously achieving the stability of the missile dynamics and accuracy of intercepting target within a desired constraint angular. Moreover, numerical simulations are exhibited to illustrate the validity of the designed control method.",
keywords = "Adaptive control, Backstepping method, Dynamic surface control, IGC, Terminal angular constraint",
author = "Ma Shichao and Li Aijun and Wang Enhe and Guo Yong and Song Danyang",
note = "Publisher Copyright: {\textcopyright} 2022, The Editor(s) (if applicable) and The Author(s), under exclusive license to Springer Nature Singapore Pte Ltd.; International Conference on Guidance, Navigation and Control, ICGNC 2020 ; Conference date: 23-10-2020 Through 25-10-2020",
year = "2022",
doi = "10.1007/978-981-15-8155-7_186",
language = "英语",
isbn = "9789811581540",
series = "Lecture Notes in Electrical Engineering",
publisher = "Springer Science and Business Media Deutschland GmbH",
pages = "2213--2225",
editor = "Liang Yan and Haibin Duan and Xiang Yu",
booktitle = "Advances in Guidance, Navigation and Control - Proceedings of 2020 International Conference on Guidance, Navigation and Control, ICGNC 2020",
}