Transducer Installation for the Sea King MK 50 Mathematical Model Validation Flight Tests.

Abstract

The installation of transducers in a R.A.N. Sea King MK 50 helicopter is described. These transducers were used to obtain flight trials data for validating a mathematical model of the aircraft. (Author)

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Document Details

Document Type
Technical Report
Publication Date
Mar 01, 1980
Accession Number
ADA089924

Entities

People

  • D. T. Hourigan

Tags

Communities of Interest

  • Air Platforms
  • Sensors

DTIC Thesaurus Topics

  • Accelerometers
  • Air Temperature
  • Aircrafts
  • Control Systems
  • Department Of Defense
  • Dynamic Pressure
  • Engineering
  • Flight Control Systems
  • Helicopters
  • Mathematical Models
  • Measurement
  • Navigational Equipment
  • Pressure Transducers
  • Rods
  • Static Pressure
  • Tail Rotors
  • Transducers

Fields of Study

  • Physics

Readers

  • Aerospace Test and Evaluation
  • Explosive Engineering.