000 | 03502nam a22005175i 4500 | ||
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001 | 978-3-642-35557-8 | ||
003 | DE-He213 | ||
005 | 20200420221256.0 | ||
007 | cr nn 008mamaa | ||
008 | 130614s2013 gw | s |||| 0|eng d | ||
020 |
_a9783642355578 _9978-3-642-35557-8 |
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024 | 7 |
_a10.1007/978-3-642-35557-8 _2doi |
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050 | 4 | _aTL787-4050.22 | |
072 | 7 |
_aTRP _2bicssc |
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072 | 7 |
_aTTDS _2bicssc |
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072 | 7 |
_aTEC002000 _2bisacsh |
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082 | 0 | 4 |
_a629.1 _223 |
245 | 1 | 2 |
_aA Combined Data and Power Management Infrastructure _h[electronic resource] : _bFor Small Satellites / _cedited by Jens Eickhoff. |
264 | 1 |
_aBerlin, Heidelberg : _bSpringer Berlin Heidelberg : _bImprint: Springer, _c2013. |
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300 |
_aXXIV, 249 p. 140 illus., 115 illus. in color. _bonline resource. |
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336 |
_atext _btxt _2rdacontent |
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337 |
_acomputer _bc _2rdamedia |
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338 |
_aonline resource _bcr _2rdacarrier |
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347 |
_atext file _bPDF _2rda |
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490 | 1 |
_aSpringer Aerospace Technology, _x1869-1730 |
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505 | 0 | _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. | |
520 | _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. | ||
650 | 0 | _aEngineering. | |
650 | 0 | _aMicroprogramming. | |
650 | 0 | _aAerospace engineering. | |
650 | 0 | _aAstronautics. | |
650 | 0 | _aElectronic circuits. | |
650 | 1 | 4 | _aEngineering. |
650 | 2 | 4 | _aAerospace Technology and Astronautics. |
650 | 2 | 4 | _aControl Structures and Microprogramming. |
650 | 2 | 4 | _aCircuits and Systems. |
700 | 1 |
_aEickhoff, Jens. _eeditor. |
|
710 | 2 | _aSpringerLink (Online service) | |
773 | 0 | _tSpringer eBooks | |
776 | 0 | 8 |
_iPrinted edition: _z9783642355561 |
830 | 0 |
_aSpringer Aerospace Technology, _x1869-1730 |
|
856 | 4 | 0 | _uhttp://dx.doi.org/10.1007/978-3-642-35557-8 |
912 | _aZDB-2-ENG | ||
942 | _cEBK | ||
999 |
_c52890 _d52890 |