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The COVE Payload - A Reconfigurable FPGA-Based Processor for CubeSatsThis paper presents the COVE payload architecture on the M-Cubed CubeSat and explores how the capabilities of this Virtex-5 FPGA-based processing platform could enable future CubeSat missions
Document ID
20120015691
Acquisition Source
Jet Propulsion Laboratory
Document Type
Conference Paper
External Source(s)
hdl:2014/42302
Authors
Bekker, Dmitriy L. (Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA, United States)
Pingree, Paula J. (Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA, United States)
Werne, Thomas A. (Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA, United States)
Wilson, Thor O. (Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA, United States)
Franklin, Brian R. (Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA, United States)
Date Acquired
August 26, 2013
Publication Date
August 8, 2011
Subject Category
Computer Programming And Software
Report/Patent Number
SSC11-I-2
Report Number: SSC11-I-2
Meeting Information
Meeting: 25th Annual AIAA/USU Conference on Small Satellites
Location: Logan, UT
Country: United States
Start Date: August 8, 2011
Sponsors: Utah State Univ., American Inst. of Aeronautics and Astronautics
Distribution Limits
Public
Copyright
Other
Keywords
multiangle-multiwavelength polarimeter
cloud and aerosol properties
on-board processing (OBP)

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