00921cam0-2200337---450-99000581220040332120131205105330.088-11-59850-8000581220FED01000581220(Aleph)000581220FED0100058122019990604d1995----km-y0itay50------baitaIT--------001yyNaturalezza del poetasaggi criticiMario Luzia cura di Giancarlo QuiricaniMilanoGarzanti1995310 p.22 cmSaggi bluPoesia801.951Luzi,Mario<1914-2005>292831Quiriconi,GiancarloITUNINARICAUNIMARCBK990005812200403321801.951 LUZ 1Dip.f.m.6840FLFBCFLFBCNaturalezza del poeta568078UNINA04342nam 22007815 450 991089019160332120250807153146.09783031655180303165518410.1007/978-3-031-65518-0(MiAaPQ)EBC31692356(Au-PeEL)EBL31692356(CKB)36231734700041(MiAaPQ)EBC31692987(Au-PeEL)EBL31692987(DE-He213)978-3-031-65518-0(OCoLC)1460294392(EXLCZ)993623173470004120240927d2024 u| 0engurcnu||||||||txtrdacontentcrdamediacrrdacarrierSpace Vehicle Maneuvering, Propulsion, Dynamics and Control A Textbook for Engineers /by Ranjan Vepa1st ed. 2024.Cham :Springer Nature Switzerland :Imprint: Springer,2024.1 online resource (553 pages)9783031655173 3031655176 Includes bibliographical references and index.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 engineeringAstronauticsOuter spaceExplorationAutomatic controlRoboticsAutomationDynamicsNonlinear theoriesAerospace Technology and AstronauticsSpace Exploration and AstronauticsControl and Systems TheoryControl, Robotics, AutomationApplied Dynamical SystemsAerospace engineering.Astronautics.Outer spaceExploration.Automatic control.Robotics.Automation.Dynamics.Nonlinear theories.Aerospace Technology and Astronautics.Space Exploration and Astronautics.Control and Systems Theory.Control, Robotics, Automation.Applied Dynamical Systems.388.13Vepa Ranjan888581MiAaPQMiAaPQMiAaPQBOOK9910890191603321Space Vehicle Maneuvering, Propulsion, Dynamics and Control4272686UNINA