LEADER 03787nam 2200661 a 450 001 9910438055103321 005 20200520144314.0 010 $a3-642-35557-9 024 7 $a10.1007/978-3-642-35557-8 035 $a(CKB)2560000000104731 035 $a(EBL)1317398 035 $a(SSID)ssj0000935373 035 $a(PQKBManifestationID)11472884 035 $a(PQKBTitleCode)TC0000935373 035 $a(PQKBWorkID)10952914 035 $a(PQKB)11741132 035 $a(DE-He213)978-3-642-35557-8 035 $a(MiAaPQ)EBC1317398 035 $a(PPN)170490610 035 $a(EXLCZ)992560000000104731 100 $a20130703d2013 uy 0 101 0 $aeng 135 $aur|n|---||||| 181 $ctxt 182 $cc 183 $acr 200 02$aA combined data and power management infrastrcture $efor small satellites /$fJens Eickhoff, editor 205 $a1st ed. 2013. 210 $aHeidelberg, Germany $cSpringer$dc2013 215 $a1 online resource (268 p.) 225 0$aSpringer aerospace technology 300 $aDescription based upon print version of record. 311 $a3-642-35556-0 320 $aIncludes bibliographical references and index. 327 $aThe OBC overall Design Concept -- The OBC Processor Board -- The I/O-Board -- The CCSDS Decoder/Encoder IP-Core -- The CCSDS Decoder/Encoder Board -- The Power Control and Distribution Unit -- The OBC Power Supply Boards -- The OBC inter-board Harness -- OBC Mechanical and Thermal Design -- OBC HW/SW Integration Testing -- The Research Satellite Target. 330 $aIn 2009 the need for a suitable onboard computer design arose for the small satellite project at the Institute of Space Systems, University of Stuttgart, Germany. It had to meet the constraints imposed by the small satellite (a 130 kg CubeSat) with its full featured ACS, diverse payloads and full CCSDS telecommand and telemetry standard compliance. The design of the Onboard Computer system lead to a functional merging between onboard computer components and the satellite's Power Control and Distribution Unit, resulting in a very innovative solution ? the so-called Combined Data and Power Management Infrastructure. The technical implementation of such a design was achieved with the support of an international industry partner consortium consisting of Astrium GmbH, Aeroflex Colorado Springs Inc., 4Links Ltd., Aeroflex Gaisler AB, Vectronic Aerospace GmbH and HEMA Kabeltechnik GmbH & Co. KG. At end of the flight unit's development the consortium decided to provide a single consistent documentation of the developed CDPI Infrastructure. The technical overview should be available for other university students in a sort of mix between technical brochure and user guide. This book also might be of interest for future university or industry partners who intend to order rebuilds / adaptations of the CDPI infrastructure or even the entire satellite bus in Stuttgart for their missions. 410 0$aSpringer Aerospace Technology,$x1869-1730 606 $aArtificial satellites$xElectronic equipment 606 $aArtificial satellites$xControl systems 606 $aEngineering 606 $aMicroprogramming 606 $aAstronautics 606 $aSystems engineering 615 0$aArtificial satellites$xElectronic equipment. 615 0$aArtificial satellites$xControl systems. 615 0$aEngineering. 615 0$aMicroprogramming. 615 0$aAstronautics. 615 0$aSystems engineering. 676 $a629.46 701 $aEickhoff$b Jens$01754893 801 0$bMiAaPQ 801 1$bMiAaPQ 801 2$bMiAaPQ 906 $aBOOK 912 $a9910438055103321 996 $aA combined data and power management infrastrcture$94191406 997 $aUNINA