04164nam a22006255i 4500 978-3-031-65518-0 DE-He213 20251030113107.0 cr nn 008mamaa 240927s2024 sz | s |||| 0|eng d 9783031655180 978-3-031-65518-0 10.1007/978-3-031-65518-0 doi TL1-4050 TRP bicssc TTDS bicssc TEC002000 bisacsh TRP thema TTDS thema Vepa, Ranjan. author. aut http://id.loc.gov/vocabulary/relators/aut 85066 Space Vehicle Maneuvering, Propulsion, Dynamics and Control [electronic resource] : A Textbook for Engineers / by Ranjan Vepa. 1st ed. 2024. Cham : Springer Nature Switzerland : Imprint: Springer, 2024. XXI, 540 p. 176 illus., 145 illus. in color. online resource. text txt rdacontent computer c rdamedia online resource cr rdacarrier text file PDF rda 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. 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 . Aerospace engineering. 66335 Astronautics. 66336 Outer space Exploration. 69043 Control engineering. Robotics. 59148 Automation. 59149 Dynamics. 65524 Nonlinear theories. 65525 Aerospace Technology and Astronautics. 66339 Space Exploration and Astronautics. 69044 Control and Systems Theory. 65868 Control, Robotics, Automation. Applied Dynamical Systems. 65530 SpringerLink (Online service) Springer Nature eBook Printed edition: 9783031655173 Printed edition: 9783031655197 Printed edition: 9783031655203 https://doi.org/10.1007/978-3-031-65518-0 ZDB-2-ENG ZDB-2-SXE 63741 63741