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020 _a9789811569906
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024 7 _a10.1007/978-981-15-6990-6
_2doi
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082 0 4 _a629.1
_223
100 1 _aXie, Yongchun.
_eauthor.
_4aut
_4http://id.loc.gov/vocabulary/relators/aut
_949550
245 1 0 _aGuidance, Navigation, and Control for Spacecraft Rendezvous and Docking: Theory and Methods
_h[electronic resource] /
_cby Yongchun Xie, Changqing Chen, Tao Liu, Min Wang.
250 _a1st ed. 2021.
264 1 _aSingapore :
_bSpringer Nature Singapore :
_bImprint: Springer,
_c2021.
300 _aXII, 495 p. 243 illus., 212 illus. in color.
_bonline resource.
336 _atext
_btxt
_2rdacontent
337 _acomputer
_bc
_2rdamedia
338 _aonline resource
_bcr
_2rdacarrier
347 _atext file
_bPDF
_2rda
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 _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. .
650 0 _aAerospace engineering.
_96033
650 0 _aAstronautics.
_949551
650 0 _aAutomotive engineering.
_949552
650 0 _aMultibody systems.
_96018
650 0 _aVibration.
_96645
650 0 _aMechanics, Applied.
_93253
650 1 4 _aAerospace Technology and Astronautics.
_949553
650 2 4 _aAutomotive Engineering.
_949554
650 2 4 _aMultibody Systems and Mechanical Vibrations.
_932157
700 1 _aChen, Changqing.
_eauthor.
_4aut
_4http://id.loc.gov/vocabulary/relators/aut
_949555
700 1 _aLiu, Tao.
_eauthor.
_4aut
_4http://id.loc.gov/vocabulary/relators/aut
_949556
700 1 _aWang, Min.
_eauthor.
_4aut
_4http://id.loc.gov/vocabulary/relators/aut
_949557
710 2 _aSpringerLink (Online service)
_949558
773 0 _tSpringer Nature eBook
776 0 8 _iPrinted edition:
_z9789811569890
776 0 8 _iPrinted edition:
_z9789811569913
776 0 8 _iPrinted edition:
_z9789811569920
856 4 0 _uhttps://doi.org/10.1007/978-981-15-6990-6
912 _aZDB-2-ENG
912 _aZDB-2-SXE
942 _cEBK
999 _c78429
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