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Computational Space Flight Mechanics

Computational Space Flight Mechanics
Kataloginformation
Feldname Details
Vorliegende Sprache eng
Hinweise auf parallele Ausgaben 330140744 Buchausg. u.d.T.: ‡Weiland, Claus, 1944 - : Computational space flight mechanics
ISBN 978-3-642-13582-8
Name Weiland, Claus
T I T E L Computational Space Flight Mechanics
Verlagsort Berlin, Heidelberg
Verlag Springer-Verlag Berlin Heidelberg
Erscheinungsjahr 2010
2010
Umfang Online-Ressource (310p. 155 illus, digital)
Reihe SpringerLink. Bücher
Notiz / Fußnoten Includes bibliographical references and index
Weiterer Inhalt Title Page; Preface; Acknowledgements; Table of Contents; Introduction; Coordinate Transformations; Transformations between Often Used Coordinate Systems; Kepler's Laws of Planetary Motion and Newton's Celestial Mechanics; The Two-Body Problem; General Equations for Planetary Flight; A Resum\'{e} of the Aerothermodynamics of Space Flight Vehicles; Three and Six Degree of Freedom Trajectory Simulations; Numerical Applications of the General Equations for Planetary Flight; The Earth Atmosphere; Solution of Problems; Appendix A; Appendix B; Appendix C; Appendix D; Appendix E; Appendix F. Name IndexSubject Index;. Cover13;Title Page -- Preface -- Acknowledgements -- Table of Contents -- Chapter 1 Introduction -- References -- Chapter 2 Coordinate Transformations -- Basic Rotational Transformations -- Time Derivative of Vectors in Moving Frames -- The Velocity Vector -- The Acceleration Vector -- The Angular Velocity in a Body Frame: Euler Angles -- Problems -- References -- Chapter 3 Transformations between Often Used Coordinate Systems -- Transformation from Geodetic to Body Frame -- Transformation from Air Path to Body Frame -- Transformation from Geodetic to Flight Path Frame -- Transformation from Planetocentric to Orbital Frame -- Problems -- References -- Chapter 4 Kepler8217;s Laws of Planetary Motion and Newton8217;s Celestial Mechanics -- Kepler8217;s 1. Law -- Kepler8217;s 2. Law -- Kepler8217;s 3. Law -- Newton8217;s Celestial Mechanics -- Problems -- References -- Chapter 5 The Two-Body Problem -- The Equation of Motion -- The Energy Conservation -- The Angular Momentum Conservation -- The Orbit Equation -- The Various Orbits -- The Eccentricity e <1 -- The Eccentricity e 8805; 1 -- Test Cases for the Three Classes of Orbits -- Time Dependency of the Orbital Variables r and 952; and Kepler8217;s Equation -- The Elliptical Orbit -- Solutions of the Elliptical Test Case 1 -- The Hyperbolic Orbit -- Solutions of the Hyperbolic Test Case 3 -- The Classical Orbital Elements -- Derivation of Relations -- Sample Calculations of Test Case 1 Using Orbital Elements -- Sample Calculations of Test Case 1 Using the General Equations of Planetary Flight -- Perturbations of Orbital Dynamics -- Lagrange8217;s Planet Equations -- Numerical Solutions of Lagrange8217;s Planet Equations -- Numerical Solution of the General Equations of Planetary Flight for an Aspherical Earth -- Problems -- References -- Chapter 6 General Equations for Planetary Flight -- Equations of Translational Motion -- Flight without Bank Angle -- Flight with Bank Angle -- Equations Including Side Forces -- Flight with Propulsion Force -- Orbital Flight Around an Aspherical Earth -- Equations of Rotational Motion -- Set of Equations for Six Degree of Freedom Simulations -- Problems -- References -- Chapter 7 A Resum'{e} of the Aerothermodynamics of Space Flight Vehicles -- Conventions for Aerothermodynamic Data -- Flow Regimes and Physical Phenomena -- Aerothermodynamic Data of the X-38 Vehicle -- Data of Longitudinal Motion -- Data of Lateral Motion -- Problems -- References -- Chapter 8 Three and Six Degree of Freedom Trajectory Simulations -- Three Degree of Freedom Simulation for a Winged Space Vehicle -- Three Degree of Freedom Simulation for a Non-Winged Space Vehicle -- Six Degree of Freedom Simulations for a Winged Space Vehicle -- Flight with Statically Stable Longitudinal Motion -- Flight with Statically Stable Longitudinal and Yaw Motion -- Problems -- References -- Chapter 9 Numerical Applications of the General Equations for Planetary Flight -- Flight in Geostationary Orbit -- Flight in Low Earth Orbit -- Circular Equatorial Orbit (Inclination Angle 966; = 0) -- Circular Orbit with Inclination Angle 966; 3;= 0 -- Elliptical Orbits -- Elliptical Orbit without Aerodynamic Forces -- Elliptical Orbit with Aerodynamic Forces -- T$29.
Titelhinweis Buchausg. u.d.T.: ‡Weiland, Claus, 1944 - : Computational space flight mechanics
ISBN ISBN 978-3-642-13583-5
Klassifikation TRP
TTDS
TEC002000
629.1
629.4
TL787-4050.22
ZO 7250
ZO 8200
Kurzbeschreibung The general practice in this book is to provide numerical solutions for all discussed topics and problems. This could be the orbit determination by the orbital elements, Lagrange's perturbation equations for disturbed Earth's orbits, the flight of a mass point in flight path coordinates (three degree of freedom), and the flight of a controlled space vehicle in body fixed coordinates (six degree of freedom). This book has been written not only for graduate and doctoral students but also for non-specialists who may be interested in this subject or concerned with space flight mechanics.
2. Kurzbeschreibung The general practice in this book is to provide numerical solutions for all discussed topics and problems. This could be the orbit determination by the orbital elements, Lagrange's perturbation equations for disturbed Earth's orbits, the flight of a mass point in flight path coordinates (three degree of freedom), and the flight of a controlled space vehicle in body fixed coordinates (six degree of freedom). This book has been written not only for graduate and doctoral students but also for non-specialists who may be interested in this subject or concerned with space flight mechanics
1. Schlagwortkette Raumflugkörper
Flugmechanik
Numerisches Verfahren
1. Schlagwortkette ANZEIGE DER KETTE Raumflugkörper -- Flugmechanik -- Numerisches Verfahren
2. Schlagwortkette Raumflugkörper
Flugmechanik
Numerisches Verfahren
ANZEIGE DER KETTE Raumflugkörper -- Flugmechanik -- Numerisches Verfahren
SWB-Titel-Idn 325492700
Signatur Springer E-Book
Bemerkungen Elektronischer Volltext - Campuslizenz
Elektronische Adresse $uhttp://dx.doi.org/10.1007/978-3-642-13583-5
Internetseite / Link Volltext
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