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Collision management utilizing CCD and remote sensing technologyWith the threat of damage to aerospace systems (space station, shuttle, hypersonic a/c, solar power satellites, loss of life, etc.) from collision with debris (manmade/artificial), there exists an opportunity for the design of a novel system (collision avoidance) to be incorporated into the overall design. While incorporating techniques from ccd and remote sensing technologies, an integrated system utilized in the infrared/visible spectrum for detection, tracking, localization, and maneuvering from doppler shift measurements is achievable. Other analysis such as impact assessment, station keeping, chemical, and optical tracking/fire control solutions are possible through this system. Utilizing modified field programmable gated arrays (software reconfiguring the hardware) the mission and mission effectiveness can be varied. This paper outlines the theoretical operation of a prototype system as it applies to collision avoidance (to be followed up by research).
Document ID
19960003777
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Mcdaniel, Harvey E., Jr.
(Princeton Univ. NJ, United States)
Date Acquired
September 6, 2013
Publication Date
September 1, 1995
Publication Information
Publication: NASA. Goddard Space Flight Center, The 1995 Shuttle Small Payloads Symposium
Subject Category
Spacecraft Design, Testing And Performance
Accession Number
96N13787
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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