NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Back to Results
The ATS-F interferometer - A precision wide field-of-view attitude sensorAn RF phase interferometer has been integrated into the ATS-F spacecraft attitude control system. Laboratory measurements indicate that the interferometer is capable of determining spacecraft attitude in pitch and roll to an accuracy of 0.18 deg over a field-of-view of plus or minus 12.5 deg about the spacecraft normal axis with an angular resolution of 0.004 deg. The system is completely solid state, weighs 17 pounds, and consumes 12.5 W of DC power.
Document ID
19740045080
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Teichman, M. A.
Marek, F. L.
Browning, J. J.
Parr, A. K.
(IBM Electronics Systems Center Gaithersburg, Md., United States)
Date Acquired
August 7, 2013
Publication Date
April 1, 1974
Subject Category
Instrumentation And Photography
Report/Patent Number
AIAA PAPER 74-486
Meeting Information
Meeting: Communications Satellite Systems Conference
Location: Los Angeles, CA
Start Date: April 22, 1974
End Date: April 24, 1974
Sponsors: American Institute of Aeronautics and Astronautics
Accession Number
74A27830
Funding Number(s)
CONTRACT_GRANT: NAS5-21100
Distribution Limits
Public
Copyright
Other

Available Downloads

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