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Image dissector camera system studyVarious aspects of a rendezvous and docking system using an image dissector detector as compared to a GaAs detector were discussed. Investigation into a gimbled scanning system is also covered and the measured video response curves from the image dissector camera are presented. Rendezvous will occur at ranges greater than 100 meters. The maximum range considered was 1000 meters. During docking, the range, range-rate, angle, and angle-rate to each reflector on the satellite must be measured. Docking range will be from 3 to 100 meters. The system consists of a CW laser diode transmitter and an image dissector receiver. The transmitter beam is amplitude modulated with three sine wave tones for ranging. The beam is coaxially combined with the receiver beam. Mechanical deflection of the transmitter beam, + or - 10 degrees in both X and Y, can be accomplished before or after it is combined with the receiver beam. The receiver will have a field-of-view (FOV) of 20 degrees and an instantaneous field-of-view (IFOV) of two milliradians (mrad) and will be electronically scanned in the image dissector. The increase in performance obtained from the GaAs photocathode is not needed to meet the present performance requirements.
Document ID
19840012738
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Howell, L.
(ITT Aerospace/Optical Div. Fort Wayne, IN, United States)
Date Acquired
September 4, 2013
Publication Date
March 1, 1984
Subject Category
Instrumentation And Photography
Report/Patent Number
NASA-CR-171759
NAS 1.26:171759
Report Number: NASA-CR-171759
Report Number: NAS 1.26:171759
Accession Number
84N20806
Funding Number(s)
CONTRACT_GRANT: NAS9-16923
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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