DocumentCode :
1501995
Title :
Attitude control — I
Author :
Farrior, J. S.
Author_Institution :
U.S. Army Ballistic Missile Agency, Huntsville, Ala.
Volume :
77
Issue :
12
fYear :
1958
Firstpage :
1084
Lastpage :
1086
Abstract :
THE PROBLEM of attitude control exists to a certain extent with all kinds of vehicles, missiles, and projectiles. Attitude control is necessary or desirable for at least the following reasons: 1. To provide mental and physical comfort for passengers. 2. To provide proper environment and positioning to allow instrumentation to function. 3. To provide proper alignment for lift surfaces and thrust vectors.
Keywords :
Aerospace electronics; Attitude control; Satellites; Space vehicles; Telescopes; Wheels;
fLanguage :
English
Journal_Title :
Electrical Engineering
Publisher :
ieee
ISSN :
0095-9197
Type :
jour
DOI :
10.1109/EE.1958.6445495
Filename :
6445495
Link To Document :
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