Experiment and study of control loading system in a flight simulator based on RCP

Zheng Shutao, Huang Qitao, Cong Dacheng, Han Junwei

科研成果: 书/报告/会议事项章节会议稿件同行评审

12 引用 (Scopus)

摘要

Control loading system is one of the important components for a flight simulator. It provides fidelity force simulation to pilot and belongs to passive force control system. According to the flight control system's principle of boeing737-300, this paper gives the simulation principle in flight simulator. Three channels Primary Control Loading system (PCL) hydraulic driven actuators were developed. The mathematical model was derived for the PCL. By means of rapid control prototyping technology, the passive force control system based on industrial personal computer is developed. Experiments demonstrate that the system has less than 4% error between computed force and actual force and good tracking performance. The PCL has been applied to flight simulator prototype system.

源语言英语
主期刊名IEEE ICIT 2007 - 2007 IEEE International Conferenceon Integration Technology
208-212
页数5
DOI
出版状态已出版 - 2007
已对外发布
活动2007 IEEE International Conference on Integration Technology, ICIT 2007 - Shenzhen, 中国
期限: 20 3月 200724 3月 2007

出版系列

姓名IEEE ICIT 2007 - 2007 IEEE International Conference on Integration Technology

会议

会议2007 IEEE International Conference on Integration Technology, ICIT 2007
国家/地区中国
Shenzhen
时期20/03/0724/03/07

指纹

探究 'Experiment and study of control loading system in a flight simulator based on RCP' 的科研主题。它们共同构成独一无二的指纹。

引用此