Stability of position-loop based hydraulic control loading system

Panguo Qi, Hui Wang, Junwei Han

科研成果: 书/报告/会议事项章节会议稿件同行评审

3 引用 (Scopus)

摘要

When flying an aircraft, the force feel of the control column provides the pilot with important information about the state of the aircraft. In a flight simulator this force feel needs to be simulated, which is the task of the control loading system. A hydraulic Control Loading System (CLS) was developed and installed on our flight simulator earlier days, but the CLS contains instabilities for some certain conditions. The stability of the CLS has been theoretically analyzed on the basis of the transfer function model founded, and a stability criterion for the CLS has been put forward, which is sufficiently proved valid by experiments. According to the stability criterion, the load mass is one of the key parameters when designing a CLS, which must be limited into a certain range in order that the CLS could operate stably.

源语言英语
主期刊名2010 International Conference on Mechanic Automation and Control Engineering, MACE2010
3363-3366
页数4
DOI
出版状态已出版 - 2010
已对外发布
活动2010 International Conference on Mechanic Automation and Control Engineering, MACE2010 - Wuhan, 中国
期限: 26 6月 201028 6月 2010

出版系列

姓名2010 International Conference on Mechanic Automation and Control Engineering, MACE2010

会议

会议2010 International Conference on Mechanic Automation and Control Engineering, MACE2010
国家/地区中国
Wuhan
时期26/06/1028/06/10

指纹

探究 'Stability of position-loop based hydraulic control loading system' 的科研主题。它们共同构成独一无二的指纹。

引用此