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Effects of Optical Artifacts in a Laser-Based Spacecraft Navigation SensorTesting of the Advanced Video Guidance Sensor (AVGS) used for proximity operations navigation on the Orbital Express ASTRO spacecraft exposed several unanticipated imaging system artifacts and aberrations that required correction to meet critical navigation performance requirements. Mitigation actions are described for a number of system error sources, including lens aberration, optical train misalignment, laser speckle, target image defects, and detector nonlinearity/noise characteristics. Sensor test requirements and protocols are described, along with a summary of test results from sensor confidence tests and system performance testing.
Document ID
20060024737
Acquisition Source
Marshall Space Flight Center
Document Type
Conference Paper
Authors
LeCroy, Jerry E.
(Boeing Co. Huntsville, AL, United States)
Hallmark, Dean S.
(Boeing Co. Huntsville, AL, United States)
Howard, Richard T.
(NASA Marshall Space Flight Center Huntsville, AL, United States)
Date Acquired
August 23, 2013
Publication Date
January 1, 2006
Subject Category
Spacecraft Instrumentation And Astrionics
Meeting Information
Meeting: SPIE Defense and Security Symposium
Location: Orlando, FL
Country: United States
Start Date: April 17, 2006
End Date: April 21, 2006
Sponsors: International Society for Optical Engineering
Distribution Limits
Public
Copyright
Other

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