@inproceedings{cf502b3509604e24a5ce4310d17d8b17,
title = "Decoupling Control Law Design for Oblique-wing Aircraft based on Eigenstructure Assignment and Model Following",
abstract = "Decoupling control law for oblique-wing aircraft (OWA) is studied. To this end, the coupling characteristicss of OWA is briefly introduced and the need to improve its flying quality through flight control is analyzed. Then a linearized flight dynamics model is built. Methods of eigenstructure assignment and model following are applied to achieve modal decoupling and dynamic decoupling respectively. Finally, F-8 OWRA (Oblique Wing Research Aircraft) is taken as a case study to demonstrate the theories built in this paper. The results indicate that both control law design methods are applicable to decouple OWA and improve its flying quality in a certain degree.",
keywords = "Decoupling control law, Eigenstructure assignment, Model following, Oblique-wing aircraft",
author = "Lu Qiu and Zhenghong Gao and Yan Liu",
note = "Publisher Copyright: {\textcopyright} 2021 32nd Congress of the International Council of the Aeronautical Sciences, ICAS 2021. All rights reserved.; 32nd Congress of the International Council of the Aeronautical Sciences, ICAS 2021 ; Conference date: 06-09-2021 Through 10-09-2021",
year = "2021",
language = "英语",
series = "32nd Congress of the International Council of the Aeronautical Sciences, ICAS 2021",
publisher = "International Council of the Aeronautical Sciences",
booktitle = "32nd Congress of the International Council of the Aeronautical Sciences, ICAS 2021",
}