@inproceedings{ab4a11e160234684bb8b4bf565aae3c4,
title = "Morphing Aircraft Flight Control Using Nonlinear Dynamic Inversion",
abstract = "This paper focuses on flight controller design for the morphing aircraft which using the swept-back wing. In this paper, the nonlinear morphing aircraft is modeled and the longitudinal mathematical equations are extracted. And the nonlinear dynamic inversion (NDI) flight controller is designed for the longitudinal mathematical model. For solving the problem of dynamic inverse error caused by modeling error in flight control, the control law is improved by adding an additional feedback in the channel of nonlinear cancellation. And to a certain extent, the influence caused by interference forces and moments and non-linear cancellation errors are eliminated. Two simulation experiments are designed for the fixed and morphing configuration. The results of them show the NDI controller has a good performance of tracing and certain robustness for the morphing aircraft.",
keywords = "Dynamic inversion, Morphing aircraft, Swept-back wing",
author = "Fuxiang Qiao and Lizhi Guo and Jingping Shi",
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_127",
language = "英语",
isbn = "9789811581540",
series = "Lecture Notes in Electrical Engineering",
publisher = "Springer Science and Business Media Deutschland GmbH",
pages = "1519--1529",
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",
}