DocumentCode :
1501999
Title :
Attitude control — II
Author :
Roberson, R. E.
Author_Institution :
Autonetics Division, North American Aviation, Inc., Downey, Calif.
Volume :
77
Issue :
12
fYear :
1958
Firstpage :
1086
Lastpage :
1088
Abstract :
CONTROLLING THE ATTITUDE of a satellite vehicle should be a simple job. The body behaves as if it were suspended on a frictionless pivot. Control torques can be small. There usually is no need for extreme precision in measurement. And adequate response times are ridiculously low by conventional servo standards.
Keywords :
Attitude control; Control systems; Equations; Flywheels; Satellites; Torque; Vehicles;
fLanguage :
English
Journal_Title :
Electrical Engineering
Publisher :
ieee
ISSN :
0095-9197
Type :
jour
DOI :
10.1109/EE.1958.6445496
Filename :
6445496
Link To Document :
بازگشت