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JWST Cryo Fine Guidance Closed Loop Test ResultsThe James Webb Space Telescope uses the Fine Guidance Controller to achieve pointing accuracy to a millionth of a degree needed for its scientific observations. This closed loop controller includes the Fine Guidance Sensor (FGS) instrument, the Attitude Control System (ACS), and the Fine Steering Mirror (FSM), all working together to generate precise attitude updates every 64 ms to stabilize and point the Observatory. It was exercised for the first time with the flight hardware during the cryogenic test at Johnson Space Center.
Document ID
20190002616
Acquisition Source
Goddard Space Flight Center
Document Type
Poster
Authors
Vila, M. Begoña
(Stinger Ghaffarian Technologies Inc. (SGT Inc.) Greenbelt, MD, United States)
Lambros, Scott D.
(Applied Technology Associates (ATA) Aerospace Greenbelt, MD, United States)
Diaz, David M.
(Northrop Grumman Aerospace Systems Redondo Beach, CA, United States)
Fu, Henry
(Northrop Grumman Aerospace Systems Redondo Beach, CA, United States)
Lee, Steven S.
(Northrop Grumman Aerospace Systems Redondo Beach, CA, United States)
Meza, Luis
(Northrop Grumman Aerospace Systems Redondo Beach, CA, United States)
Phillips, Kevin J.
(Microtel LLC Greenbelt, MD, United States)
del Rosario, Ben
(Northrop Grumman Aerospace Systems Redondo Beach, CA, United States)
Wu, J. Carl
(Hammers Co. Greenbelt, MD, United States)
Date Acquired
April 19, 2019
Publication Date
June 10, 2018
Subject Category
Astronomy
Instrumentation And Photography
Report/Patent Number
GSFC-E-DAA-TN56789
Report Number: GSFC-E-DAA-TN56789
Meeting Information
Meeting: SPIE Astronomical Telescopes + Instrumentation
Location: Austin, TX
Country: United States
Start Date: June 10, 2018
End Date: June 15, 2018
Sponsors: International Society for Optical Engineering
Funding Number(s)
CONTRACT_GRANT: NAS5-02200
CONTRACT_GRANT: NNG15CR64C
Distribution Limits
Public
Copyright
Public Use Permitted.
Technical Review
Single Expert
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