@inproceedings{46b47092ab8d40a4ac2b3ef9548ad4bc,
title = "Research on aerodynamically assisted orbit maneuver method based on feature model correction",
abstract = "For the hypersonic vehicle to use aerodynamic assistance to carry out orbit maneuver, because of the considerable uncertainty in the aerodynamic parameters during the re-entry process, how to carry out precise orbit maneuver with aerodynamic assistance is an important part of the research of this method. Using predictive correction guidance and control methods based on feature models, fixed-cycle track prediction and guidance correction during flight can greatly improve the robustness and adaptive ability of the system and eliminate the control deviation caused by uncertain aerodynamic parameters and allow the vehicle to accurately determine the orbit. A model with parametric bias was established for system simulation. The results show that the accuracy of the guidance control still meets the system requirements and the system has good selfadaptability through this method with aerodynamic parameter bias of 40\%.",
keywords = "Adaptive control, Aerodynamically assisted, Model-based, Orbit maneuver",
author = "Yue Lin and Yingmin Jia and Songtao Fan",
note = "Publisher Copyright: {\textcopyright} The Editor(s) (if applicable) and The Author(s), under exclusive license to Springer Nature Singapore Pte Ltd. 2021.; Chinese Intelligent Systems Conference, CISC 2020 ; Conference date: 24-10-2020 Through 25-10-2020",
year = "2021",
doi = "10.1007/978-981-15-8450-3\_60",
language = "英语",
isbn = "9789811584497",
series = "Lecture Notes in Electrical Engineering",
publisher = "Springer Science and Business Media Deutschland GmbH",
pages = "569--578",
editor = "Yingmin Jia and Weicun Zhang and Yongling Fu",
booktitle = "Proceedings of 2020 Chinese Intelligent Systems Conference - Volume I",
address = "德国",
}