Sea King Mk. 50 Helicopter Flight Control System. A Mathematical Model of the Flying Controls

Abstract

A mathematical model for the flying controls of the Sea King Ozark-50 helicopter is presented. The operation of the systems and components used in the flying controls of the aircraft is described first, followed by a detailed description of the construction and functioning of the mathematical model. Equations and diagrams for the model are included.

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Document Details

Document Type
Technical Report
Publication Date
Feb 01, 1979
Accession Number
ADA086529

Entities

People

  • Christopher R. Guy

Tags

Communities of Interest

  • Space

DTIC Thesaurus Topics

  • Aerodynamics
  • Aeronautical Laboratories
  • Air Force
  • Aircrafts
  • Airframes
  • Angular Acceleration
  • Computer Programs
  • Construction
  • Control Systems
  • Department Of Defense
  • Engineering
  • Equations
  • Flight Control Systems
  • Helicopters
  • Mathematical Models
  • Models
  • Tail Rotors

Fields of Study

  • Biology
  • Physics

Readers

  • Aerospace Engineering
  • Control Systems Engineering.