@inproceedings{f7909fb2fbe648948e90a6b89e9fe1c3,
title = "C* Control Law for Longitudinal Maneuvering of Fly-by-Wire Receiver Aircraft During Aerial Refueling",
abstract = "Piloted receiver aircrafts are most common type of aircrafts which get refueled in flight for increasing its flight range. This paper stresses an essential technical problem related to the controller design during aerial refueling process intended for piloted receiver aircraft equipped with fly-by-wire flight control system (FBW-FCS), which is the typical symbol of modern airplanes. Considering the fact that pilot is sensitive to norm overload and angular velocity during the flight, the proposed C* control law in longitudinal channel receives the pilot{\textquoteright}s joystick movement as input as well as normal overload and pitch angular velocity as feedback signals for smoothly aviating the aircrafts with good feelings. An attitude boundary protection method is also introduced to ensure the flying safety. Simulation results manifest that the proposed C* control law is effective for controlling norm overload with great transition performance.",
keywords = "Aerial refueling, C* control law, Normal overload",
author = "Cihang Wu and Jianguo Yan and Jiawei Wang and Yiming Guo and Yaohong Qu",
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_389",
language = "英语",
isbn = "9789811581540",
series = "Lecture Notes in Electrical Engineering",
publisher = "Springer Science and Business Media Deutschland GmbH",
pages = "4709--4719",
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",
}