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An Improvement of PWPF in Reaction Control System of Hypersonic Vehicle

  • Jia Song*
  • , Likun Bian
  • *此作品的通讯作者
  • Beihang University

科研成果: 书/报告/会议事项章节会议稿件同行评审

摘要

Attitude control of hypersonic vehicles (HVs) when they just reenter the atmosphere almost rely on their reaction control systems (RCS). However, modulation is needed in RCS because RCS is a discrete system. There are three usual modulators which are used in RCS. They are Bang-bang control, pulse width modulation (PWM) and pulse width pulse frequency modulation (PWPF). We analyzed the pseudo-linear and other characteristics of three modulators in this paper, as a result, PWPF has better pseudo-linear performance and better step response but more switching times. So, we proposed one new PWPF by add a damping coefficient in feedback to reduce switching times of PWPF. The new PWPF has a better step response performance and smaller switching frequency than traditional PWPF. Finally, we use simulation verify the feasibility of the new PWPF.

源语言英语
主期刊名Proceedings of 2019 Chinese Intelligent Systems Conference - Volume III
编辑Yingmin Jia, Junping Du, Weicun Zhang
出版商Springer Verlag
169-178
页数10
ISBN(印刷版)9789813296978
DOI
出版状态已出版 - 2020
活动Chinese Intelligent Systems Conference, CISC 2019 - Haikou, 中国
期限: 26 10月 201927 10月 2019

出版系列

姓名Lecture Notes in Electrical Engineering
594
ISSN(印刷版)1876-1100
ISSN(电子版)1876-1119

会议

会议Chinese Intelligent Systems Conference, CISC 2019
国家/地区中国
Haikou
时期26/10/1927/10/19

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