INVESTIGATION OF X-11 NOSE CONE ATTITUDE CONTROL SYSTEM IN PITCH,

Abstract

A preliminary investigation, in pitch alone, was made to determine approximate values of the system parameters. In this memorandum, the pitch equations, corresponding analog computer circuits and the results of the investigation are presented. From these results, estimates of the design parameters for the Model X-11 nose cone attitude control system are determined. (Author)

Document Details

Document Type
Technical Report
Publication Date
May 30, 1954
Accession Number
AD0834022

Entities

People

  • H. T. Wexler
  • J. Beharrell

Organizations

  • General Dynamics

Tags

DTIC Thesaurus Topics

  • Air Traffic Control Systems
  • Analog Computers
  • Attitude Control Systems
  • Computers
  • Computing Devices
  • Control Systems
  • Entry Control Systems
  • Equations
  • Flight Control Systems
  • Nose Cones
  • Noses

Fields of Study

  • Physics

Readers

  • Aerodynamics/Aeronautics.
  • Aerospace Test and Evaluation
  • Computational Modeling and Simulation