Controllability Analysis of the Autopilot with Angular-Acceleration Feedback

Yuhui Hu, Kai Shen*, K. A. Neusypin, Jingyu Shi, Jingzhong Zheng

*此作品的通讯作者

科研成果: 书/报告/会议事项章节会议稿件同行评审

1 引用 (Scopus)

摘要

With the advantages in direct measurement and control of the flight overload and its change rate, feedback of angular acceleration has become perspective for the flight control system of high maneuvering aircrafts. In this contribution, an enhanced acceleration autopilot with the angular acceleration feedback is designed for the pitch channel of tail-controlled missiles. The linear quadratic approach is implemented to determine the feedback gain of two-loop autopilots. To investigate the superiority of the angular acceleration feedback over the traditional angular rate feedback, a criterion named degree of output controllability (DOC) has been modified for evaluating the output controllability of the system with different feedback constructures. Stability and controllability analysis is carried out through numerical simulations for both kinds of autopilots with different static stability properties. The results show that the static instability and the feedback of angular acceleration is able to enhance the controllability of the two-loop autopilot.

源语言英语
主期刊名Advances in Guidance, Navigation and Control - Proceedings of 2022 International Conference on Guidance, Navigation and Control
编辑Liang Yan, Haibin Duan, Yimin Deng, Liang Yan
出版商Springer Science and Business Media Deutschland GmbH
859-868
页数10
ISBN(印刷版)9789811966125
DOI
出版状态已出版 - 2023
活动International Conference on Guidance, Navigation and Control, ICGNC 2022 - Harbin, 中国
期限: 5 8月 20227 8月 2022

出版系列

姓名Lecture Notes in Electrical Engineering
845 LNEE
ISSN(印刷版)1876-1100
ISSN(电子版)1876-1119

会议

会议International Conference on Guidance, Navigation and Control, ICGNC 2022
国家/地区中国
Harbin
时期5/08/227/08/22

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