RESULTS OF A STUDY TO DETERMINE THE EFFECTS OF ROTARY HYDRAULIC ACTUATORS ON THE FLIGHT CONTROL SYSTEM, STABILITY, AND DESIGN,

Abstract

The report describes an evaluation of rotary hydraulic actuators for use on aircraft flight control systems.

Document Details

Document Type
Technical Report
Publication Date
Oct 03, 1957
Accession Number
AD0682146

Entities

People

  • P. E. Russell

Organizations

  • General Dynamics

Tags

Communities of Interest

  • Air Platforms

DTIC Thesaurus Topics

  • Actuators
  • Air Traffic Control Systems
  • Aircrafts
  • Control Systems
  • Flight Control Systems
  • Hydraulic Actuators
  • Mechanical Equipment
  • Pneumatic Equipment
  • Test And Evaluation

Fields of Study

  • Physics

Readers

  • Robotics and Automation.