NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Back to Results
Space telescope pointing control systemThe Space Telescope is a free-flying spacecraft designed for Space Shuttle launch. The Space Telescope's pointing control system slews the optical axis from one target star region of the celestial sphere to the next, and maintains precision pointing for the target star for up to 24 hours. The spacecraft digital computer processes the precision attitude and rate sensor data to generate torque commands for the reaction wheels. The pointing control system has four major elements: the command generator, the control system, the attitude reference processing, and momentum management. The emphasis is on relating design requirements to the hardware and software implementation.
Document ID
19820054905
Acquisition Source
Legacy CDMS
Document Type
Reprint (Version printed in journal)
Authors
Dougherty, H.
(Lockheed Missiles and Space Co., Inc. Space System Div., Sunnyvale, CA, United States)
Tompetrini, K.
(Lockheed Missiles and Space Co. Sunnyvale, CA, United States)
Levinthal, J.
(Bendix Corp. Guidance Systems Div., Teterboro, NJ, United States)
Nurre, G.
(NASA Marshall Space Flight Center System Dynamics Laboratory, Huntsville, AL, United States)
Date Acquired
August 10, 2013
Publication Date
August 1, 1982
Subject Category
Spacecraft Instrumentation
Report/Patent Number
AIAA PAPER 80-1784
Report Number: AIAA PAPER 80-1784
Accession Number
82A38440
Funding Number(s)
CONTRACT_GRANT: NAS8-32697
Distribution Limits
Public
Copyright
Other

Available Downloads

There are no available downloads for this record.
No Preview Available