| 000 | 03597nam a22005775i 4500 | ||
|---|---|---|---|
| 001 | 978-3-319-25540-8 | ||
| 003 | DE-He213 | ||
| 005 | 20220801222201.0 | ||
| 007 | cr nn 008mamaa | ||
| 008 | 151027s2016 sz | s |||| 0|eng d | ||
| 020 |
_a9783319255408 _9978-3-319-25540-8 |
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| 024 | 7 |
_a10.1007/978-3-319-25540-8 _2doi |
|
| 050 | 4 | _aTL1-4050 | |
| 072 | 7 |
_aTRP _2bicssc |
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| 072 | 7 |
_aTTDS _2bicssc |
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_aTEC002000 _2bisacsh |
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_aTRP _2thema |
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_aTTDS _2thema |
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| 082 | 0 | 4 |
_a629.1 _223 |
| 100 | 1 |
_aMazzini, Leonardo. _eauthor. _4aut _4http://id.loc.gov/vocabulary/relators/aut _960153 |
|
| 245 | 1 | 0 |
_aFlexible Spacecraft Dynamics, Control and Guidance _h[electronic resource] : _bTechnologies by Giovanni Campolo / _cby Leonardo Mazzini. |
| 250 | _a1st ed. 2016. | ||
| 264 | 1 |
_aCham : _bSpringer International Publishing : _bImprint: Springer, _c2016. |
|
| 300 |
_aXXI, 363 p. _bonline resource. |
||
| 336 |
_atext _btxt _2rdacontent |
||
| 337 |
_acomputer _bc _2rdamedia |
||
| 338 |
_aonline resource _bcr _2rdacarrier |
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| 347 |
_atext file _bPDF _2rda |
||
| 490 | 1 |
_aSpringer Aerospace Technology, _x1869-1749 |
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| 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. | |
| 520 | _aThis book is an up-to-date compendium on spacecraft attitude and orbit control (AOC) that offers a systematic and complete treatment of the subject with the aim of imparting the theoretical and practical knowledge that is required by designers, engineers, and researchers. After an introduction on the kinematics of the flexible and agile space vehicles, the modern architecture and functions of an AOC system are described and the main AOC modes reviewed with possible design solutions and examples. The dynamics of the flexible body in space are then considered using an original Lagrangian approach suitable for the control applications of large space flexible structures. Subsequent chapters address optimal control theory, attitude control methods, and orbit control applications, including the optimal orbital transfer with finite and infinite thrust. The theory is integrated with a description of current propulsion systems, with the focus especially on the new electric propulsion systems and state of the art sensors and actuators. | ||
| 650 | 0 |
_aAerospace engineering. _96033 |
|
| 650 | 0 |
_aAstronautics. _960154 |
|
| 650 | 0 |
_aControl engineering. _931970 |
|
| 650 | 0 |
_aSolar system. _932100 |
|
| 650 | 1 | 4 |
_aAerospace Technology and Astronautics. _960155 |
| 650 | 2 | 4 |
_aControl and Systems Theory. _931972 |
| 650 | 2 | 4 |
_aSpace Physics. _932102 |
| 710 | 2 |
_aSpringerLink (Online service) _960156 |
|
| 773 | 0 | _tSpringer Nature eBook | |
| 776 | 0 | 8 |
_iPrinted edition: _z9783319255385 |
| 776 | 0 | 8 |
_iPrinted edition: _z9783319255392 |
| 776 | 0 | 8 |
_iPrinted edition: _z9783319368771 |
| 830 | 0 |
_aSpringer Aerospace Technology, _x1869-1749 _960157 |
|
| 856 | 4 | 0 | _uhttps://doi.org/10.1007/978-3-319-25540-8 |
| 912 | _aZDB-2-ENG | ||
| 912 | _aZDB-2-SXE | ||
| 942 | _cEBK | ||
| 999 |
_c80487 _d80487 |
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