Decoupling Control Law Design for Oblique-wing Aircraft based on Eigenstructure Assignment and Model Following

Lu Qiu, Zhenghong Gao, Yan Liu

科研成果: 书/报告/会议事项章节会议稿件同行评审

摘要

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.

源语言英语
主期刊名32nd Congress of the International Council of the Aeronautical Sciences, ICAS 2021
出版商International Council of the Aeronautical Sciences
ISBN(电子版)9783932182914
出版状态已出版 - 2021
活动32nd Congress of the International Council of the Aeronautical Sciences, ICAS 2021 - Shanghai, 中国
期限: 6 9月 202110 9月 2021

出版系列

姓名32nd Congress of the International Council of the Aeronautical Sciences, ICAS 2021

会议

会议32nd Congress of the International Council of the Aeronautical Sciences, ICAS 2021
国家/地区中国
Shanghai
时期6/09/2110/09/21

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