DocumentCode
1226823
Title
Torque Coupled Bang Bang Attitude Control
Author
Axelband, Elliot I.
Volume
12
Issue
2
fYear
1965
fDate
6/1/1965 12:00:00 AM
Firstpage
129
Lastpage
133
Abstract
The properties of gas jet torque coupled attitude control in the design context of a coast phase attitude control system for a nonatmospheric planetary landing space vehicle are discussed.
Keywords
Aerospace control; Aerospace electronics; Aircraft navigation; Attitude control; Brightness; Equations; Fuels; Sensor systems; Space vehicles; Sun;
fLanguage
English
Journal_Title
Aerospace and Navigational Electronics, IEEE Transactions on
Publisher
ieee
ISSN
0096-1957
Type
jour
DOI
10.1109/TANE.1965.4319324
Filename
4319324
Link To Document