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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.
Preface
List of Abbreviations
Celestial Mechanics: Keplerian Orbits
Celestial Mechanics: Real Orbits
Space Vehicle Manoeuvring
Interplanetary Trajectories
Space Vehicle Mission Planning
Trajectory Optimization and Feedback Control
Patched Three-Body Approximation: Application to Interplanetary Trajectory Planning
Missions to the Asteroids
Physics of Plasmas
Space Vehicle Electric Propulsion
Space Vehicle Electro-static and Electro-magnetic Propulsion
Space Vehicle Electro-dynamic Propulsion
Index