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_a10.1007/978-981-15-6990-6 _2doi |
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_aES-MaUEC _bspa _cES-MaUEC _erda _dES-MaUEC |
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_aTL795 _b2021 EB |
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| 100 | 1 |
_aXie, Yongchun _eautor _4aut _4http://id.loc.gov/vocabulary/relators/aut _9678498 |
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| 245 | 1 | 0 |
_aGuidance, Navigation, and Control for Spacecraft Rendezvous and Docking : _bTheory and Methods _cby Yongchun Xie, Changqing Chen, Tao Liu, Min Wang |
| 250 | _aFirst edition 2021 | ||
| 264 | 1 |
_aSingapore _bSpringer International Publishing _c2021 |
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| 300 |
_a1 recurso en línea (XII, 495 páginas) _b243 ilustraciones, 212 ilustraciones a color |
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_aarchivo de texto _bPDF |
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| 490 | 0 | _aEngineering (SpringerNature-11647) | |
| 490 | 0 | _aEngineering (R0) (SpringerNature-43712) | |
| 505 | 0 | _aIntroduction -- Rendezvous Kinematics and Dynamics -- Navigation Meathod and Schematic Design for Rendezvous and Docking -- Guidance Meathod and Schematic Design for Rendezvous and Docking -- Automatic Control Method and Scheme Design for Rendezvous and Docking -- Manual Control Method and Scheme Design for Rendezvous and Docking -- Theory and Design of Thruster Configuration and Control Allocation -- Method and Scheme Design of Safety for Rendezvous and Docking -- Simulation Verification of Rendezvous and Docking -- RVD Verification in Orbit Flight. | |
| 520 | 3 | _aThis book focuses on the theory of and design methods for guidance, navigation, and control (GNC) in the context of spacecraft rendezvous and docking (RVD). The position and attitude dynamics and kinematics equations for RVD are presented systematically and in accordance with several different coordinate systems, including elliptical orbital frame, and recommendations are supplied on which of these equations to use in different phases of RVD. The book subsequently explains the basic principles and relative navigation algorithms of RVD sensors such as GNSS, radar, and camera-type RVD sensors. It also provides guidance algorithms and schemes for different phases of RVD, including the latest research advances in rapid RVD. In turn, the book presents a detailed introduction to intelligent adaptive control and proposes corresponding theoretical approaches to thruster configuration and control allocation for RVD. Emphasis is placed on the design method of active and passive trajectory protection in different phases of RVD, and on the safety design of the RVD mission as a whole. For purposes of verification, the Shenzhou spacecraft's in-orbit flight mission is presented as well. All issues addressed are described and explained from basic principles to detailed engineering methods and examples, providing aerospace engineers and students both a basic understanding of, and numerous practical engineering methods for, GNC system design in RVD. . | |
| 988 | _aSpringer_Engineering_2021 | ||
| 650 | 7 |
_2embne _9139696 _aVehículos espaciales |
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| 650 | 7 |
_2embne _9138156 _aAstronáutica |
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| 700 | 1 |
_aChen, Changqing _eautor _4aut _4http://id.loc.gov/vocabulary/relators/aut _9678499 _d1946- |
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| 700 | 1 |
_aLiu, Tao _eautor _4aut _4http://id.loc.gov/vocabulary/relators/aut _9678500 |
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| 700 | 1 |
_aWang, Min _eautor _4aut _4http://id.loc.gov/vocabulary/relators/aut _9678501 |
|
| 856 | 4 | 0 |
_uhttps://go.openathens.net/redirector/universidadeuropea.es?url=https://doi.org/10.1007/978-981-15-6990-6 _zAcceso a este recurso digital (usuarios Universidad Europea de Madrid) |
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