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TIROS-N spacecraft jitter calculationsThe TIROS-N television infrared observatory system is discussed. The characteristics of the primary payload sensor are presented. The attitude control system jitter specification for satisfactory performance of the sensor is analyzed. The primary sensor is the advanced very high resolution radiometer. The TIROS-N satellite is an orbital platform carrying a number of earth observation sensors. The requirements for three axis attitude control for proper positioning of the sensors are reported.
Document ID
19730011159
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Fleisher, G. M. (NASA Goddard Space Flight Center Greenbelt, MD, United States)
Date Acquired
September 2, 2013
Publication Date
December 1, 1972
Subject Category
Space Vehicles
Report/Patent Number
NASA-TM-X-66201
X-732-73-51
Accession Number
73N19886
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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