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The COVE Payload - A Reconfigurable FPGA-Based Processor for CubeSats
External Online Source: hdl:2014/42302
Author and Affiliation:
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)
Abstract: This 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
Publication Date: Aug 08, 2011
Document ID:
20120015691
(Acquired Nov 16, 2012)
Subject Category: COMPUTER PROGRAMMING AND SOFTWARE
Report/Patent Number: SSC11-I-2
Document Type: Conference Paper
Meeting Information: 25th Annual AIAA/USU Conference on Small Satellites; 8 Aug. 2011; Logan, UT; United States
Meeting Sponsor: American Inst. of Aeronautics and Astronautics; United States
Utah State Univ.; Logan, UT, United States
Financial Sponsor: Jet Propulsion Lab., California Inst. of Tech.; Pasadena, CA, United States
Organization Source: Jet Propulsion Lab., California Inst. of Tech.; Pasadena, CA, United States
Description: 10p; In English; Original contains color illustrations
Distribution Limits: Unclassified; Publicly available; Unlimited
Rights: Copyright
NASA Terms: FIELD-PROGRAMMABLE GATE ARRAYS; PAYLOADS; CENTRAL PROCESSING UNITS; ARCHITECTURE (COMPUTERS); COMPUTER PROGRAMS; INTEGRATED CIRCUITS
Other Descriptors: ON-BOARD PROCESSING (OBP); MULTIANGLE-MULTIWAVELENGTH POLARIMETER; CLOUD AND AEROSOL PROPERTIES
Availability Source: Other Sources
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