LONGITUDINAL EQUATIONS OF MOTION FOR TILT WING-TILT PROP VTOL AIRCRAFT.

Abstract

The report summarizes a derivation of the longitudinal equations of motion for a tilt wing - tilt prop aircraft in transition for flight simulation purposes. (Author)

Document Details

Document Type
Technical Report
Publication Date
Dec 12, 1966
Accession Number
AD0684038

Entities

People

  • Robert T. Chen

Organizations

  • Boeing Rotorcraft Systems

Tags

Communities of Interest

  • Air Platforms

DTIC Thesaurus Topics

  • Aircrafts
  • Equations
  • Equations Of Motion
  • Flight Simulations
  • Simulations
  • Simulators
  • Tilt Wings
  • Transitions
  • Vehicles

Fields of Study

  • Physics

Readers

  • Aerospace Engineering
  • Control Systems Engineering.