Development and Flight Test of an Advanced Hydrofluidic Stabilization System

Abstract

The objective of this program is to demonstrate the performance of an advanced hydrofluidic stabilization system that is designed to provide pilot relief modes within a highly reliable, low-cost system. The system was designed, built, and tested to obtain the desired performance, and then subjected to flightworthiness testing to ensure structural integrity. The system was then installed, flight tested, and evaluated in a UH-1M helicopter. The flight test results are discussed.

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Document Details

Document Type
Technical Report
Publication Date
Feb 01, 1976
Accession Number
ADA023466

Entities

People

  • Darroll Bengtson
  • James Hedeen
  • Robert Helfinstine

Organizations

  • Honeywell International, Inc.

Tags

Communities of Interest

  • Air Platforms
  • Energy and Power Technologies
  • Sensors
  • Space
  • Weapons Technologies

DTIC Thesaurus Topics

  • Aircrafts
  • Control Panels
  • Control Systems
  • Dynamic Pressure
  • Dynamic Response
  • Electrical Circuits
  • Electronic Circuits
  • Failure Mode And Effect Analysis
  • Field Effect Transistors
  • Flight Control Systems
  • Fluidic Amplifiers
  • Pressure Regulators
  • Pressure Transducers
  • Resonant Frequency
  • Stabilization Systems
  • Test And Evaluation
  • Transducers

Readers

  • Aerospace Engineering
  • Software Engineering