Fly-by-Wire versus Dual Mechanical Controls for the Advanced Scout Helicopter - Quantitative Comparison

Abstract

A preliminary design study comparing fly-by-wire with dual mechanical controls for the Advanced Scout Helicopter was conducted by Bell Helicopter Textron. The purpose was to determine if significant payoffs were available in the utilization of fly-by-wire design concepts. Considered were flight safety and mission reliability; vulnerability; system reliability, availability, and maintainability; control system weight; electrical and hydraulic power supply requirements; initial and life-cycle costs; and predicted handling qualities. In addition, the study investigated the payoffs from the use of innovative thinking relative to cockpit controls.

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Document Details

Document Type
Technical Report
Publication Date
Jan 01, 1981
Accession Number
ADA096089

Entities

People

  • Gaylord W. Carlock
  • Kenneth F. Guinn

Organizations

  • Bell Flight

Tags

Communities of Interest

  • Advanced Electronics
  • Air Platforms
  • Cyber
  • Sensors
  • Weapons Technologies

DTIC Thesaurus Topics

  • Actuators
  • Air Force
  • Aircrafts
  • Control Sticks
  • Control Systems
  • Explosions
  • Explosive Charges
  • Explosives
  • Failure Mode And Effect Analysis
  • Flight Control Systems
  • Fuselages
  • Inertial Navigation
  • Inertial Navigation Systems
  • Plastic Explosives
  • Processing Equipment
  • Transducers
  • Warning Systems

Readers

  • Aviation Science / Aeronautics.
  • Life Cycle Cost Analysis
  • Reinforced Composite Materials