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Space vehicle maneuvering, propulsion, dynamics and control = a textbook for engineers /

紀錄類型:	書目-語言資料,印刷品 : Monograph/item
正題名/作者:	Space vehicle maneuvering, propulsion, dynamics and control/ by Ranjan Vepa.
其他題名:	a textbook for engineers /
作者:	Vepa, Ranjan.
出版者:	Cham :Springer Nature Switzerland : : 2024.,
面頁冊數:	xxi, 540 p. :ill. (some col.), digital ; : 24 cm.;
Contained By:	Springer Nature eBook
標題:	Space vehicles - Propulsion systems. -
電子資源:	https://doi.org/10.1007/978-3-031-65518-0
ISBN:	9783031655180

Space vehicle maneuvering, propulsion, dynamics and control = a textbook for engineers /
Vepa, Ranjan.

Space vehicle maneuvering, propulsion, dynamics and controla textbook for engineers /[electronic resource] :by Ranjan Vepa. - Cham :Springer Nature Switzerland :2024. - xxi, 540 p. :ill. (some col.), digital ;24 cm.

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.

ISBN: 9783031655180

Standard No.: 10.1007/978-3-031-65518-0doiSubjects--Topical Terms:

671284
Space vehicles
--Propulsion systems.

LC Class. No.: TL782

Dewey Class. No.: 629.475

Space vehicle maneuvering, propulsion, dynamics and control = a textbook for engineers /
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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.
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