AIRCRAFT FLIGHT CONTROL ACTUATION SYSTEM DESIGN
This book describes the earliest flight control actuation systems and their progression from aerodynamic tab-controlled surfaces to mechanical-input-controlled hydraulic actuators to electrical-input-controlled fly-by-wire actuation systems (both hydraulic and electromechanical). The book also covers: Alternate Command Systems; Electrically Powered (Power-By-Wire) Actuation Systems; Flight Control System Design Requirements; Applicable Specifications and Advisory Documents; Power Control Unit and Power-Drive Unit Design Guidelines; Dynamic Performance and Response; PCU Assembly and Installation; and Quality Assurance.
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Availability:
- Find a library where document is available. Order URL: http://worldcat.org/isbn/1560913762
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Corporate Authors:
Society of Automotive Engineers (SAE)
400 Commonwealth Drive
Warrendale, PA United States 15096 -
Authors:
- Raymond, E T
- Chenoweth, C C
- Publication Date: 1993
Language
- English
Media Info
- Pagination: 286 p.
Subject/Index Terms
- TRT Terms: Actuated traffic signal controllers; Airborne navigational aids; Aircraft pilotage; Flight control systems; Hydraulic equipment
- Uncontrolled Terms: Aircraft instruments
- Old TRIS Terms: Actuated control; Hydraulic control
- Subject Areas: Aviation; Vehicles and Equipment;
Filing Info
- Accession Number: 00732064
- Record Type: Publication
- ISBN: 1560913762
- Report/Paper Numbers: R-123
- Files: TRIS
- Created Date: Feb 4 1997 12:00AM