LEADER 04342nam 22007815 450 001 9910890191603321 005 20250807153146.0 010 $a9783031655180 010 $a3031655184 024 7 $a10.1007/978-3-031-65518-0 035 $a(MiAaPQ)EBC31692356 035 $a(Au-PeEL)EBL31692356 035 $a(CKB)36231734700041 035 $a(MiAaPQ)EBC31692987 035 $a(Au-PeEL)EBL31692987 035 $a(DE-He213)978-3-031-65518-0 035 $a(OCoLC)1460294392 035 $a(EXLCZ)9936231734700041 100 $a20240927d2024 u| 0 101 0 $aeng 135 $aurcnu|||||||| 181 $ctxt$2rdacontent 182 $cc$2rdamedia 183 $acr$2rdacarrier 200 10$aSpace Vehicle Maneuvering, Propulsion, Dynamics and Control $eA Textbook for Engineers /$fby Ranjan Vepa 205 $a1st ed. 2024. 210 1$aCham :$cSpringer Nature Switzerland :$cImprint: Springer,$d2024. 215 $a1 online resource (553 pages) 311 08$a9783031655173 311 08$a3031655176 320 $aIncludes bibliographical references and index. 327 $aChapter 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. 330 $aThis 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 . 606 $aAerospace engineering 606 $aAstronautics 606 $aOuter space$xExploration 606 $aAutomatic control 606 $aRobotics 606 $aAutomation 606 $aDynamics 606 $aNonlinear theories 606 $aAerospace Technology and Astronautics 606 $aSpace Exploration and Astronautics 606 $aControl and Systems Theory 606 $aControl, Robotics, Automation 606 $aApplied Dynamical Systems 615 0$aAerospace engineering. 615 0$aAstronautics. 615 0$aOuter space$xExploration. 615 0$aAutomatic control. 615 0$aRobotics. 615 0$aAutomation. 615 0$aDynamics. 615 0$aNonlinear theories. 615 14$aAerospace Technology and Astronautics. 615 24$aSpace Exploration and Astronautics. 615 24$aControl and Systems Theory. 615 24$aControl, Robotics, Automation. 615 24$aApplied Dynamical Systems. 676 $a388.13 700 $aVepa$b Ranjan$0888581 801 0$bMiAaPQ 801 1$bMiAaPQ 801 2$bMiAaPQ 906 $aBOOK 912 $a9910890191603321 996 $aSpace Vehicle Maneuvering, Propulsion, Dynamics and Control$94272686 997 $aUNINA