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.

Language

  • English

Media Info

  • Pagination: 286 p.

Subject/Index Terms

Filing Info

  • Accession Number: 00732064
  • Record Type: Publication
  • ISBN: 1560913762
  • Report/Paper Numbers: R-123
  • Files: TRIS
  • Created Date: Feb 4 1997 12:00AM