System developed by Ling-Temco-Vought, Inc for Electric Propulsion Space Test System project (WS-661A); principal characteristics of concept and key features; concept, intended as actuation device for attitude control, incorporates features making it possible to be used as measuring device to measure torques imparted to space vehicle; installation and construction considerations; advantages include availability of direct, accurate readout of applied torque, use of off-the-shelf components, good dynamic response characteristics, redundancy, low power requirements, and low weight for angular momentum capacity.
Twin gyro attitude control system designed for disturbance instrumentation of space vehicle
SAE -- Paper
SAE Meeting ; 1964 Control
1964
6 pages
Aufsatz (Konferenz)
Englisch
© Metadata Copyright Elsevier B. V. All rights reserved.
A Twin Gyro Attitude Control System Designed for Disturbance Instrumentation of a Space Vehicle
SAE Technical Papers | 1964
|Twin-gyro attitude control systems.
AIAA | 1966
|Results of studies on twin-gyro attitude-control system for space vehicles
Engineering Index Backfile | 1964
|