Simulation and analysis of the dynamic characteristics of the internally carried air-launched aircraft

Xiao Long Zheng, Shuo Tang

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

1 Scopus citations

Abstract

To ensure the security of the entire air-launched carrier rockets system is an important issue in the research work. As the most expensive part of the system, the numerical simulation of the dynamic characteristics of the aircraft plays an important role. Dynamic equations of aircraft and its cargo during flight are derived in detail and dynamic models are established in accordance to the basic principles of theoretical mechanics and flight dynamics. The dynamic models are then utilized for the simulation of the process of the system. By comparing the simulation results and the real flight test measurements, the models are verified to be correct and precise. The dynamic characteristic of the aircraft under various conditions is also analyzed.

Original languageEnglish
Title of host publicationCAR 2010 - 2010 2nd International Asia Conference on Informatics in Control, Automation and Robotics
Pages242-245
Number of pages4
DOIs
StatePublished - 2010
Event2010 2nd International Asia Conference on Informatics in Control, Automation and Robotics, CAR 2010 - Wuhan, China
Duration: 6 Mar 20107 Mar 2010

Publication series

NameCAR 2010 - 2010 2nd International Asia Conference on Informatics in Control, Automation and Robotics
Volume3

Conference

Conference2010 2nd International Asia Conference on Informatics in Control, Automation and Robotics, CAR 2010
Country/TerritoryChina
CityWuhan
Period6/03/107/03/10

Keywords

  • Air-launch
  • Carrier rocket
  • Dynamic characteristic
  • Simulation

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