Reliability and Redundancy Study for Electronic Flight Control Systems.

Abstract

This report contains the results of a three-part study relating to development of electronic (fly-by-wire) flight control systems. Flight safety and mission reliability goals for fly-by-wire flight control systems were derived based on a survey of Navy-supplied data on operational aircraft. Electronics augmentation equipment was surveyed to determine achieved reliability on this equipment. Correlation factors were derived for reliability predictions to achieve better accuracy in prediction techniques for electronic systems. Three basic fly-by-wire system mechanizations were studied. Relative merits of each were determined, particularly with respect to monitoring and built-in test functions. Design criteria were developed for a selected configuration. (Author)

Document Details

Document Type
Technical Report
Publication Date
Jul 01, 1972
Accession Number
AD0902445

Entities

People

  • Gordon L. Seller
  • Lyle L. Montague
  • Robert F. Helfinstine

Organizations

  • Honeywell International, Inc.

Tags

Communities of Interest

  • Air Platforms

DTIC Thesaurus Topics

  • Accuracy
  • Aircrafts
  • Control Systems
  • Design Criteria
  • Electronic Equipment
  • Electronics
  • Flight Control Systems
  • Mechanization
  • Monitoring
  • Redundancy
  • Reliability
  • Vehicle Equipment
  • Vehicles

Fields of Study

  • Engineering
  • Physics

Readers

  • Inertial Navigation Systems.
  • Software Engineering

Technology Areas

  • Microelectronics
  • Microelectronics - Microelectromechanical Systems