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001 978-3-031-65518-0
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008 240927s2024 sz | s |||| 0|eng d
020 _a9783031655180
_9978-3-031-65518-0
024 7 _a10.1007/978-3-031-65518-0
_2doi
050 4 _aTL1-4050
072 7 _aTRP
_2bicssc
072 7 _aTTDS
_2bicssc
072 7 _aTEC002000
_2bisacsh
072 7 _aTRP
_2thema
072 7 _aTTDS
_2thema
100 1 _aVepa, Ranjan.
_eauthor.
_4aut
_4http://id.loc.gov/vocabulary/relators/aut
_985066
245 1 0 _aSpace Vehicle Maneuvering, Propulsion, Dynamics and Control
_h[electronic resource] :
_bA Textbook for Engineers /
_cby Ranjan Vepa.
250 _a1st ed. 2024.
264 1 _aCham :
_bSpringer Nature Switzerland :
_bImprint: Springer,
_c2024.
300 _aXXI, 540 p. 176 illus., 145 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 _aChapter 1 Celestial Mechanics: Keplerian Orbits -- Chapter 2 Celestial Mechanics: Real Orbits -- Chapter 3 Space Vehicle Manoeuvring -- Chapter 4 Interplanetary Trajectories -- Chapter 5 Space Vehicle Mission Planning -- Chapter 6 Trajectory Optimisation and Feedback Control -- Chapter 7 Patched Three-Body Approximation: Application to Inter-Planetary Trajectory Planning -- Chapter 8 Missions to the Asteroids -- Chapter 9 Physics of Plasmas -- Chapter 10 Space Vehicle Electric Propulsion -- Chapter 11 Space Vehicle Electro-Static and Electro-Magnetic Propulsion -- Chapter 12 Space Vehicle Electro-Dynamic Propulsion.
520 _aThis textbook introduces space vehicle maneuvering, propulsion, dynamics and control, and discusses the space environment and its influence on the spacecraft propulsion system. This is followed by an in depth description of Keplerian celestial mechanics, co-planar and non-planar orbital transfers involving both impulsive and continuous manoeuvers, and perturbation effects that characterize the real non-Keplerian nature of orbital motion. Dr. Vepa then explains the use of restricted two-body and three-body dynamics as descriptors of spacecraft motion, the limitations of these approach in terms of orbital perturbations and an understanding of the physical source and influence of these perturbations, and principles of the optimal synthesis of trajectories. Featuring many exercises, design case studies, and extensive use of MATLAB/SIMULINK and MATLAB analytical tools, the book is ideal for graduate students, post graduate students, researchers, as well professionals in the industry. Stands as a single, ready reference for all that would be required for design of a specific or a complete space mission; Explains the basics of celestial mechanics including Keplerian, Real and Non-Keplerian Orbits; Illustrates the principles of maneuvering vehicles in space, optimal trajectories, and space vehicle mission planning .
650 0 _aAerospace engineering.
_966335
650 0 _aAstronautics.
_966336
650 0 _aOuter space
_xExploration.
_969043
650 0 _aControl engineering.
650 0 _aRobotics.
_959148
650 0 _aAutomation.
_959149
650 0 _aDynamics.
_965524
650 0 _aNonlinear theories.
_965525
650 1 4 _aAerospace Technology and Astronautics.
_966339
650 2 4 _aSpace Exploration and Astronautics.
_969044
650 2 4 _aControl and Systems Theory.
_965868
650 2 4 _aControl, Robotics, Automation.
650 2 4 _aApplied Dynamical Systems.
_965530
710 2 _aSpringerLink (Online service)
773 0 _tSpringer Nature eBook
776 0 8 _iPrinted edition:
_z9783031655173
776 0 8 _iPrinted edition:
_z9783031655197
776 0 8 _iPrinted edition:
_z9783031655203
856 4 0 _uhttps://doi.org/10.1007/978-3-031-65518-0
912 _aZDB-2-ENG
912 _aZDB-2-SXE
999 _c63741
_d63741