Space Vehicle Maneuvering, Propulsion, Dynamics and Control A Textbook for Engineers /

This 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 in...

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Autor principal: Vepa, Ranjan (Author)
Autor Corporativo: SpringerLink (Online service)
Formato: Recurso Electrónico livro electrónico
Idioma:inglês
Publicado em: Cham : Springer Nature Switzerland : Imprint: Springer, 2024.
Edição:1st ed. 2024.
Assuntos:
Acesso em linha:https://doi.org/10.1007/978-3-031-65518-0
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250 |a 1st ed. 2024. 
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505 0 |a Chapter 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 |a This 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 . 
532 8 |a Accessibility summary: This PDF does not fully comply with PDF/UA standards, but does feature limited screen reader support, described non-text content (images, graphs), bookmarks for easy navigation and searchable, selectable text. Users of assistive technologies may experience difficulty navigating or interpreting content in this document. We recognize the importance of accessibility, and we welcome queries about accessibility for any of our products. If you have a question or an access need, please get in touch with us at accessibilitysupport@springernature.com. 
532 8 |a No reading system accessibility options actively disabled 
532 8 |a Publisher contact for further accessibility information: accessibilitysupport@springernature.com 
588 |a Print version record. 
650 0 |a Aerospace engineering. 
650 0 |a Astronautics. 
650 0 |a Outer space  |x Exploration. 
650 0 |a Control engineering. 
650 0 |a Robotics. 
650 0 |a Automation. 
650 0 |a Dynamics. 
650 0 |a Nonlinear theories. 
650 1 4 |a Aerospace Technology and Astronautics. 
650 2 4 |a Space Exploration and Astronautics. 
650 2 4 |a Control and Systems Theory. 
650 2 4 |a Control, Robotics, Automation. 
650 2 4 |a Applied Dynamical Systems. 
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912 |a ZDB-2-SXE 
950 |a Engineering (SpringerNature-11647) 
950 |a Engineering (R0) (SpringerNature-43712)