Test Evaluation of a Reconfigurable Fault-Tolerant Fly-By-Wire Actuation System

Abstract

The system was designed to be two-fail-operate for electromechanical failures and single-fail-operate for hydromechanical failures. The system used a single microprocessor to close the position control loop, monitor the operation of the actuator and reconfigure the system upon component failures of the actuator. The microprocessor was not designed to be failure tolerant. The testing conducted was a measurement of the input-to-output characteristics of the system. The system was unusual in the use of a microprocessor for failure detection and control and in that electro-hydraulic channels were operated together in a nominal force fight configuration. The test evaluation included operating the system in both loaded and unloaded configurations. The system operated successfully with input/output characteristics similar to other fly-by- wire systems. Areas where improvements or careful design should be implemented are presented in the report.

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Document Details

Document Type
Technical Report
Publication Date
Jul 08, 1986
Accession Number
ADA172455

Entities

People

  • Gavin D. Jenney
  • Julianne Minch
  • William G. Talley

Tags

Communities of Interest

  • Advanced Electronics
  • Energy and Power Technologies

DTIC Thesaurus Topics

  • Actuators
  • Aeronautical Laboratories
  • Air Force
  • Bias
  • Control Systems
  • Damage Detection
  • Detection
  • Failure Mode And Effect Analysis
  • Frequency Response
  • Measurement
  • Operating Systems
  • Performance Tests
  • Rdx
  • Reliability
  • Self Assembly
  • Test And Evaluation
  • Waveforms

Fields of Study

  • Physics

Readers

  • Integrated Circuit Design and Technology.
  • Robotics and Automation.
  • Structural Health Monitoring of Composite Structures.

Technology Areas

  • Microelectronics
  • Microelectronics - Microelectromechanical Systems