@inproceedings{318caf2d249742d397acba041f359fa5,
title = "Design of Carrier-Based Aircraft Landing Control Law Based on Direct Force",
abstract = "Direct Force can eliminate the coupling between the force and moment, directly produce the force to change the trajectory of plane, it can improve carrier-based aircraft{\textquoteright}s landing quality and efficiency. This paper will discuss the application of direct force and thrust vector technology based on F-16 aircraft model. Firstly, we discussed how thrust vector produce force and moment on airplane, and using thrust vector to apply direct force control on plane. Secondly, we design the dynamic inversion control and combine the control distribution technology to achieve inner loop control. Lastly, we design the direct lift model landing control law and the path angle rate model control law, the simulation results show that the path angle rate mode landing responses are more rapid.",
keywords = "Direct force, Dynamic inversion, Landing control, Thrust Vector",
author = "Hongyuan Zhu and Xiaoxiong Liu and Zhang, {Yue Hang} and Yu Li",
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_96",
language = "英语",
isbn = "9789811581540",
series = "Lecture Notes in Electrical Engineering",
publisher = "Springer Science and Business Media Deutschland GmbH",
pages = "1153--1163",
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",
}