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Design constraints of the LST fine guidance sensorThe LST Fine Guidance Sensor design is shaped by the rate of occurrence of suitable guide stars, the competition for telescope focal plane space with the Science Instruments, and the sensitivity of candidate image motion sensors. The relationship between these parameters is presented, and sensitivity to faint stars is shown to be of prime importance. An interferometric technique of image motion sensing is shown to have improved sensitivity and, therefore, a reduced focal plane area requirement in comparison with other candidate techniques (image-splitting prism and image dissector tube techniques). Another design requirement is speed in acquiring the guide star in order to maximize the time available for science observations. The design constraints are shown parametrically, and modelling results are presented.
Document ID
19750057566
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Wissinger, A. B.
(Perkin-Elmer Corp. Norwalk, Conn., United States)
Date Acquired
August 8, 2013
Publication Date
August 1, 1975
Subject Category
Space Communications, Spacecraft Communications, Command And Tracking
Report/Patent Number
AIAA PAPER 75-1072
Meeting Information
Meeting: American Institute of Aeronautics and Astronautics, Guidance and Control Conference
Location: Boston, MA
Start Date: August 20, 1975
End Date: August 22, 1975
Sponsors: American Institute of Aeronautics and Astronautics
Accession Number
75A41638
Funding Number(s)
CONTRACT_GRANT: NAS8-29948
Distribution Limits
Public
Copyright
Other

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