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TSIS Experiences with ISS Jitter from Inception to On-Orbit OperationThe TSIS instrument has been measuring solar irradiance on a continual basis since January 2018 as an external payload on the ISS. In 2014 when TSIS was directed to fly on the ISS, the jitter environment was highly uncertain, so TSIS designed a robust gimbaled pointing system that showed excellent disturbance attenuation throughout the design, test, and on-orbit phases of the program. This paper discusses how TSIS accounted for this uncertain jitter environment through-out the life of the program.TSIS was able to measure the ISS jitter during commissioning and determined that it was a relatively benign environment less than 4 arcseconds 1σ at low frequencies (<0.5 Hz). More importantly, the measured pointing performance of TSIS was consistently found to be 4 arcseconds 1σ, which easily satisfied the jitter requirement of 60 arcseconds 1σ.
Document ID
20190000637
Acquisition Source
Goddard Space Flight Center
Document Type
Conference Paper
Authors
Brown, Patrick
(Colorado Univ. Boulder, CO, United States)
Engelmann, Andrew
(Colorado Univ. Boulder, CO, United States)
Date Acquired
February 11, 2019
Publication Date
January 31, 2019
Subject Category
Engineering (General)
Report/Patent Number
GSFC-E-DAA-TN64840
Report Number: GSFC-E-DAA-TN64840
Meeting Information
Meeting: AAS Annual Guidance and Control Conference
Location: Breckenridge, CO
Country: United States
Start Date: February 1, 2019
End Date: February 6, 2019
Sponsors: American Astronautical Society
Funding Number(s)
CONTRACT_GRANT: 80GSFC18C0056
Distribution Limits
Public
Copyright
Public Use Permitted.
Keywords
solar irradiance instrument
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