@inproceedings{814901b9ba2a4d50ad4434ab3736c2c1,
title = "Nonsingular Fast Terminal Sliding Mode Based Impact Angle Guidance Law",
abstract = "In traditional guidance law, target maneuver is always considered an external disturbance with known boundary. This paper proposed an impact angle constraint guidance law for intercepting maneuvering targets via NFTSM. It can drive the tracking error and light of sight (LOS) angle rate to zero. Unlike most technologies, the proposed guidance law can effectively avoid undesired chatter without any performance sacrifice. The stability and converge feature are analyzed via construct Lyapunov function is given. Numerical simulation demonstrates that compared with the traditional NTSM, the guidance law proposed in this paper can achieve more accurate interception in a more extensive interception angle range, and the overall performance is better.",
keywords = "Impact angle constraint, Missile guidance, Nonsingular fast terminal sliding mode, Target maneuvering",
author = "Bailin Chen and Shiyao Lin and Guang Zhang and Junzhi Li and Wang Wei",
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_346",
language = "English",
isbn = "9789811966125",
series = "Lecture Notes in Electrical Engineering",
publisher = "Springer Science and Business Media Deutschland GmbH",
pages = "3567--3576",
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 = "Germany",
}