DocumentCode
1120914
Title
Precision Stabilization Systems
Author
Rue, A.K.
Author_Institution
Hughes Aircraft Company Culver City, Calif.
Issue
1
fYear
1974
Firstpage
34
Lastpage
42
Abstract
This paper discusses the relationships that must be considered in analyzing the design and performance of typical precision stabilization systems. In particular, the disturbance inputs that are due to kinematic and geometrical coupling are examined in depth by considering systems implemented with either a conventional two-axis gimbal or a traditional half-angle mirror assembly. The disturbance coupling that is associated with the gimbal drive actuators and the effect of structural compliance on the stabilization control loops are also discussed in detail. Other aspects of stabilization system design that are considered include the potential improvements in performance that can be achieved by using appropriate multiaxis gimbal configurations and by utilizing the angular pointing characterisitics of beam expansion telescopes.
Keywords
Actuators; Assembly systems; Drives; Friction; Infrared sensors; Kinematics; Mirrors; Sensor phenomena and characterization; Torque; Tracking;
fLanguage
English
Journal_Title
Aerospace and Electronic Systems, IEEE Transactions on
Publisher
ieee
ISSN
0018-9251
Type
jour
DOI
10.1109/TAES.1974.307961
Filename
4101160
Link To Document