Definition Study for an Advanced Fighter Digital Flight Control System

Abstract

The Definition Study for an Advanced Fighter Digital Flight Control System is an exploratory definition study of which a principal objective is to derive and evaluate custom multimode control laws, related displays, and multichannel digital fly-by-wire implementation schemes for advanced Air Force and Navy fighters. Study results show that a triplex flight control system provides the lowest weight, the best maintainability, and the lowest cost of the candidate configurations considered. Results also indicate that mission-oriented flight control laws integrated with compatible displays and controllers can provide enhanced mission effectiveness and reduced pilot workload. It is recommended that the concepts analyzed and simulated during this definition study be implemented and evaluated by flight testing.

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Document Details

Document Type
Technical Report
Publication Date
Jun 01, 1975
Accession Number
ADB006024

Entities

People

  • David S. Hooker
  • George J. Vetsch
  • George R. Smith
  • Ira G. Pope

Organizations

  • McDonnell Aircraft Corporation

Tags

Communities of Interest

  • Air Platforms
  • Energy and Power Technologies
  • Ground and Sea Platforms
  • Sensors
  • Space
  • Weapons Technologies

DTIC Thesaurus Topics

  • Aircraft Equipment
  • Aircrafts
  • Airframes
  • Computer Programming
  • Computer Programs
  • Computers
  • Control Surfaces
  • Control Systems
  • Data Processing
  • Detectors
  • Engineers
  • Failure Mode And Effect Analysis
  • Inertial Navigation
  • Inertial Navigation Systems
  • Information Processing
  • Military Aircraft
  • Test And Evaluation

Readers

  • Aviation Science / Aeronautics.
  • Software Engineering