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| 003 | MX-SnUAN | ||
| 005 | 20160429161542.0 | ||
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| 008 | 160111s2016 gw | s |||| 0|eng d | ||
| 020 |
_a9783319255408 _9978-3-319-25540-8 |
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| 035 | _avtls000422740 | ||
| 039 | 9 |
_y201601111028 _zstaff |
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| 050 | 4 | _aTL787-4050.22 | |
| 100 | 1 |
_aMazzini, Leonardo, _eautor. _9367793 |
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| 245 | 1 | 0 |
_aFlexible spacecraft dynamics, control and guidance : _btechnologies by giovanni campolo / _cLeonardo Mazzini. |
| 250 | _a1st ed. 2016. | ||
| 264 | 1 |
_aCham : _bSpringer International Publishing : _bSpringer, _c2016. |
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| 300 |
_axxi, 363 páginas : _b154 ilustraciones, 20 ilustraciones en color. |
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| 336 |
_atexto _btxt _2rdacontent |
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| 337 |
_acomputadora _bc _2rdamedia |
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| 338 |
_arecurso en línea _bcr _2rdacarrier |
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| 347 |
_aarchivo de texto _bPDF _2rda |
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| 490 | 0 |
_aSpringer Aerospace Technology, _x1869-1730 |
|
| 500 | _aSpringer eBooks | ||
| 505 | 0 | _aIntroduction -- The Kinematic of the flexible satellite -- The Satellite Attitude Control System -- The Dynamic of the flexible body -- The Dynamic in the Gravitational Field -- The Optimal Control Theory -- Attitude Control Methods -- Orbital Dynamic and Control -- Spacecraft Propulsion -- Sensors and Actuators technologies -- Complements to Body Kinematic -- Elements of Estimation Theory -- Basics of Lagrangian Equations -- The J2 perturbation solution -- Complements to Optimal Orbital Transfer -- Elements of Plasma physics. | |
| 590 | _aPara consulta fuera de la UANL se requiere clave de acceso remoto. | ||
| 710 | 2 |
_aSpringerLink (Servicio en línea) _9299170 |
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| 776 | 0 | 8 |
_iEdición impresa: _z9783319255385 |
| 856 | 4 | 0 |
_uhttp://remoto.dgb.uanl.mx/login?url=http://dx.doi.org/10.1007/978-3-319-25540-8 _zConectar a Springer E-Books (Para consulta externa se requiere previa autentificación en Biblioteca Digital UANL) |
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