Helicopter roll on takeoff simulation

Jacob Enciu, A. Rosen

Research output: Chapter in Book/Report/Conference proceedingConference contribution

Abstract

Six degrees of freedom simulation of helicopter roll on takeoff is described. The simulation incorporates helicopter and landing gear dynamic models, as well as a simplified human pilot model which is capable of performing the takeoff process in various ambient and runway conditions, and for different helicopter configurations. This simulation is used in order to evaluate roll on takeoff distances and carry out a simplified preliminary optimization in order to define takeoff techniques that reduce the roll on takeoff distances.

Original languageEnglish (US)
Title of host publication49th Israel Annual Conference on Aerospace Sciences 2009
Pages348-369
Number of pages22
StatePublished - Dec 1 2009
Event49th Israel Annual Conference on Aerospace Sciences 2009 - Tel Aviv and Haifa, Israel
Duration: Mar 4 2009Mar 5 2009

Publication series

Name49th Israel Annual Conference on Aerospace Sciences 2009
Volume1

Conference

Conference49th Israel Annual Conference on Aerospace Sciences 2009
CountryIsrael
CityTel Aviv and Haifa
Period3/4/093/5/09

All Science Journal Classification (ASJC) codes

  • Computer Science(all)
  • Space and Planetary Science
  • Energy Engineering and Power Technology
  • Aerospace Engineering
  • Physics and Astronomy(all)

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  • Cite this

    Enciu, J., & Rosen, A. (2009). Helicopter roll on takeoff simulation. In 49th Israel Annual Conference on Aerospace Sciences 2009 (pp. 348-369). (49th Israel Annual Conference on Aerospace Sciences 2009; Vol. 1).