跳到主要导航 跳到搜索 跳到主要内容

Dnamics analysis of aircraft landing on the pitching deck

  • Zhen Qing Wang*
  • , Xiao Yu Sun
  • , Song Zhou
  • , Hong Shuai Lei
  • *此作品的通讯作者
  • Harbin Engineering University

科研成果: 书/报告/会议事项章节 › 会议稿件 › 同行评审

摘要

In order to study the aircraft landing on the deck, the landing(on or off center) dynamics model of airplane on deck is built.In this model,the interactions of the aircraft landing attitude, the arresting force acting on the aircraft are considered,and the influence of dynamic deck is introduced into the model.The deck coordinate system is put forward to solve the complex simulation problem.At last,by simulation,it is demonstrated that the model can be applied to the aircraft landing attitude,it is also proved that the model is comprehensive and suitable for any abnormal landing situation.

源语言英语
主期刊名Materials, Mechatronics and Automation
出版商Trans Tech Publications Ltd.
页579-582
页数4
ISBN(印刷版)9783037850176
DOI
出版状态已出版 - 2011
已对外发布是

丛书

姓名Key Engineering Materials
卷467-469
ISSN(印刷版)1013-9826
ISSN(电子版)1662-9795

学术指纹

探究 'Dnamics analysis of aircraft landing on the pitching deck' 的科研主题。它们共同构成独一无二的学术指纹。

引用此