@inproceedings{71abba0be1394063a1f83f29798c25f1,
title = "Terminal velocity and impact angle control based on generalized polynomial guidance",
abstract = "This paper proposes a novel approach to control terminal velocity and impact angle during a missile's descent phase using a simple dynamic model. This approach involves obtaining the acceleration control command from the generalized polynomial after normalizing the residual range. Then the gradient descent method is used to predict the terminal velocity and adjust the guidance parameters. Finally, numerical simulation results show that the approach achieves the guidance objective under various constraints of terminal velocity and impact angle through.",
keywords = "generalized polynomial guidance, gradient descent, impact angle control, terminal velocity control",
author = "Jiajun Wu and Jinping Li and Xijing Hu and Hao Xu and Shilei Zhao and Liangyu Zhao",
note = "Publisher Copyright: {\textcopyright} 2023 IEEE.; 38th Youth Academic Annual Conference of Chinese Association of Automation, YAC 2023 ; Conference date: 27-08-2023 Through 29-08-2023",
year = "2023",
doi = "10.1109/YAC59482.2023.10401740",
language = "English",
series = "Proceedings - 2023 38th Youth Academic Annual Conference of Chinese Association of Automation, YAC 2023",
publisher = "Institute of Electrical and Electronics Engineers Inc.",
pages = "457--462",
booktitle = "Proceedings - 2023 38th Youth Academic Annual Conference of Chinese Association of Automation, YAC 2023",
address = "United States",
}