Dnamics analysis of aircraft landing on the pitching deck

Zhen Qing Wang*, Xiao Yu Sun, Song Zhou, Hong Shuai Lei

*Corresponding author for this work

Research output: Chapter in Book/Report/Conference proceedingConference contributionpeer-review

4 Citations (Scopus)

Abstract

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.

Original languageEnglish
Title of host publicationMaterials, Mechatronics and Automation
PublisherTrans Tech Publications Ltd.
Pages579-582
Number of pages4
ISBN (Print)9783037850176
DOIs
Publication statusPublished - 2011
Externally publishedYes

Publication series

NameKey Engineering Materials
Volume467-469
ISSN (Print)1013-9826
ISSN (Electronic)1662-9795

Keywords

  • Aircraft landing
  • Arresting force
  • Dynamics model
  • Landing situation
  • Simulation problem

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