Disturbance Observer-Based Fixed-Time Attitude Autopilot for Guided Projectile

Hongyan Zhang, Shiyao Lin, Yuchan Wang, Wei Wang*

*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

摘要

In this paper, a robust attitude autopilot for spinning glide guided projectile is presented. Combing with the idea of trajectory linearization control (TLC), a TLC based fixed-time converged integral sliding mode control scheme is present. Moreover, to estimate and compensate total uncertainties, a reduced-order extended state observer is developed. The stability of closed-loop system is verified via Lyapunov method. Finally, numerical simulation is carried out to demonstrate the efficiency of proposed attitude autopilot.

源语言英语
主期刊名Proceedings of 2023 IEEE International Conference on Unmanned Systems, ICUS 2023
编辑Rong Song
出版商Institute of Electrical and Electronics Engineers Inc.
58-63
页数6
ISBN(电子版)9798350316308
DOI
出版状态已出版 - 2023
活动2023 IEEE International Conference on Unmanned Systems, ICUS 2023 - Hefei, 中国
期限: 13 10月 202315 10月 2023

出版系列

姓名Proceedings of 2023 IEEE International Conference on Unmanned Systems, ICUS 2023

会议

会议2023 IEEE International Conference on Unmanned Systems, ICUS 2023
国家/地区中国
Hefei
时期13/10/2315/10/23

指纹

探究 'Disturbance Observer-Based Fixed-Time Attitude Autopilot for Guided Projectile' 的科研主题。它们共同构成独一无二的指纹。

引用此