| 000 | 02796nam a22003615i 4500 | ||
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| 001 | 395171 | ||
| 003 | ES-MaUEC | ||
| 005 | 20230110120127.0 | ||
| 007 | cr nn 008mamaa | ||
| 008 | 210915s2022 si | s |||| 0|eng d | ||
| 020 | _a9789811650970 | ||
| 024 | 7 |
_a10.1007/978-981-16-5097-0 _2doi |
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| 040 |
_aES-MaUEC _bspa _cES-MaUEC |
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| 100 | 1 |
_aWang, Jie. _eauthor. _4aut _4http://id.loc.gov/vocabulary/relators/aut |
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| 245 | 1 | 0 |
_aRigid-Flexible Coupling Dynamics and Control of Flexible Spacecraft with Time-Varying Parameters _cby Jie Wang, Dong-Xu Li. |
| 250 | _a1st edition 2022 | ||
| 264 | 1 |
_aSingapore _bSpringer International Publishing _c2022 |
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| 300 |
_a1 recurso en línea (IX, 185 páginas) _b159 ilustraciones, 108 ilustraciones a color |
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| 336 |
_atexto _btxt _2rdacontent |
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| 337 |
_aelectrónico _bc _2rdamedia |
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| 338 |
_arecurso electrónico _bcr _2rdacarrier |
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| 347 |
_aarchivo de texto _bPDF |
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| 505 | 0 | _aIntroduction -- Modeling of Flexible Spacecraft with Time-varying Parameters -- Dynamic Analysis of Flexible Spacecraft with Time-varying Parameters -- Vibration Control Methods for Systems in Complex Mode Space -- Optimal Variable Amplitudes Input Shaping Control for Slew Maneuver of Flexible Spacecraft -- Coupling Control Method for Flexible Spacecraft -- Attitude Coupling Control Experiments -- Future. | |
| 520 | _aThis book presents the dynamic modeling and attitude control of flexible spacecraft with time-varying parameters. The dynamic characteristics, vibration control methods and attitude stabilization methods for spacecraft are systematically studied in respects of the theoretical modeling, numerical simulation and the ground experiment. Three active control theories in complex mode space are presented for flexible space structures. Optimal slew strategies based on variable amplitudes input shaping methods and coupling control methods are proposed for stabilization of flexible spacecraft. The research provides an important way to solve the problem of high-precision attitude control of flexible spacecraft with time-varying parameters. This book is appropriate for the researchers who focus on the multi-body dynamics, attitude and vibration control of flexible spacecraft. | ||
| 776 | 0 | 8 |
_iPrinted edition: _z9789811650963 |
| 776 | 0 | 8 |
_iPrinted edition: _z9789811650987 |
| 776 | 0 | 8 |
_iPrinted edition: _z9789811650994 |
| 856 | 4 | 0 |
_uhttps://go.openathens.net/redirector/universidadeuropea.es?url=https://doi.org/10.1007/978-981-16-5097-0 _zAcceso a este recurso digital (usuarios Universidad Europea de Madrid) |
| 942 |
_2lcc _cLE |
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| 988 | _aSpringer_Robotics_2022 | ||
| 999 |
_c395171 _d395171 |
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