Sun Tracker Evaluation Tests of the Centaur Attitude Control System.

Abstract

The objective of the tests was to determine the control system stable limit cycle characteristics in each of the pitch and yaw planes, with the sun tracking system enabled. (Author)

Document Details

Document Type
Technical Report
Publication Date
Nov 07, 1961
Accession Number
AD0843151

Entities

People

  • R. Pytlewski

Organizations

  • General Dynamics

Tags

Communities of Interest

  • Air Platforms

DTIC Thesaurus Topics

  • Air Traffic Control Systems
  • Attitude Control Systems
  • Control Systems
  • Entry Control Systems
  • Flight Control Systems
  • Test And Evaluation

Readers

  • Aerodynamics/Aeronautics.
  • Aerospace Test and Evaluation
  • Solar Physics