Electromechanical Actuation Development Program (EADP). Power Control Development.

Abstract

Electromechanical actuation of primary flight control surfaces has been demonstrated by the development of an integrated rotary hingeline dual-redundant actuation unit. Improved system bandwidth was demonstrated after employing improved sensors and electronic controls. (Author)

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Document Details

Document Type
Technical Report
Publication Date
Sep 01, 1981
Accession Number
ADA116126

Entities

People

  • David Bailey
  • Robert Belanus
  • Stephen Rowe

Tags

Communities of Interest

  • Advanced Electronics
  • Air Platforms
  • Sensors

DTIC Thesaurus Topics

  • Aerodynamic Control Surfaces
  • Aeronautical Laboratories
  • Air Force
  • Aircraft Equipment
  • Aircrafts
  • Contracts
  • Control Surfaces
  • Control Systems
  • Dc Motors
  • Electric Motors
  • Frequency
  • Frequency Response
  • Manufacturing
  • Motors
  • Surfaces
  • Test And Evaluation
  • Test Equipment

Readers

  • Robotics and Automation.
  • Systems Analysis and Design

Technology Areas

  • Microelectronics
  • Microelectronics - Microelectromechanical Systems