Investigation of control and stability augmentation requirements for tandem tilting ducted propeller VTOL transports

Abstract

Theoretical and analog computer investigations were conducted to determine the control and stability augmentation requirements for tandem tilting ducted propeller VTOL transports. The type of aircraft considered had performance capabilities similar to those required for the Tri-Service VTOL transport.

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Document Details

Document Type
Technical Report
Publication Date
Jul 01, 1963
Accession Number
AD0419126

Entities

People

  • David P. Miller
  • James W. Clark
  • Robert A. Gallant

Organizations

  • United Technologies Corporation

Tags

Communities of Interest

  • Air Platforms
  • Space
  • Weapons Technologies

DTIC Thesaurus Topics

  • Adaptive Control Systems
  • Aerodynamic Characteristics
  • Aircraft Equipment
  • Aircrafts
  • Airframes
  • Computer Programs
  • Computer Simulations
  • Control Systems
  • Engineers
  • Fixed Wing Aircraft
  • Flight Simulators
  • Flight Speeds
  • Research Aircraft
  • Rotary Wing Aircraft
  • Short Takeoff Aircraft
  • Shrouded Propellers
  • Wind Tunnels

Readers

  • Aerodynamics.
  • Aerospace Test and Evaluation
  • Ocean-Atmosphere Mesoscale Modeling, Data Assimilation, and Flux Boundary Layers