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Detalles Bibliográficos
Clasificación:Libro Electrónico
Otros Autores: Chobotov, Vladimir A.
Formato: Electrónico eBook
Idioma:Inglés
Publicado: Reston, Va. : American Institute of Aeronautics and Astronautics, ©2002.
Edición:3rd ed.
Colección:AIAA education series.
Temas:
Orbital mechanics.
Artificial satellites > Orbits.
Navigation (Astronautics)
Mécanique orbitale.
Satellites artificiels > Orbites.
Navigation (Astronautique)
Acceso en línea:Texto completo
Tabla de Contenidos:
  • Cover
  • Title
  • Copyright
  • Foreword
  • Preface
  • About the Authors
  • Table of Contents
  • Chapter 1. Basic Concepts
  • 1.1 A Historical Perspective
  • 1.2 Velocity and Acceleration
  • Problems
  • Selected Solutions
  • Chapter 2. Celestial Relationships
  • 2.1 Coordinate Systems
  • 2.2 Time Systems
  • References
  • Chapter 3. Keplerian Orbits
  • 3.1 Newton's Universal Law of Gravitation
  • 3.2 General and Restricted Two-Body Problem
  • 3.3 Conservation of Mechanical Energy
  • 3.4 Conservation of Angular Momentum
  • 3.5 Orbital Parameters of a Satellite3.6 Orbital Elements
  • References
  • Problems
  • Selected Solutions
  • Chapter 4. Position and Velocity as a Function of Time
  • 4.1 General Relationships
  • 4.2 Solving Kepler's Equation
  • 4.3 A Universal Approach
  • 4.4 Expressions with f and g
  • 4.5 Summary of the Universal Approach
  • 4.6 The Classical Element Set
  • 4.7 The Rectangular Coordinate System
  • 4.8 Modified Classical to Cartesian Transformation
  • 4.9 Rectangular to Modified Classical Elements Transformation
  • 4.10 The Spherical (ADBARV) Coordinate System4.11 Rectangular to Spherical Transformation
  • 4.12 Spherical to Rectangular Transformation
  • 4.13 The Earth-Relative Spherical (LDBARV) Coordinate System
  • 4.14 Geodetic and Geocentric Altitudes
  • 4.15 Converting from Perigee/Apogee Radii to Perigee/Apogee Altitudes
  • 4.16 Converting from Perigee/Apogee Altitudes to Perigee/Apogee Radii
  • References
  • Problems
  • Selected Solutions
  • Chapter 5. Orbital Maneuvers
  • 5.1 Orbital Energy
  • 5.2 Single-Impulse Maneuvers
  • 5.3 Single- and Two-Impulse Transfer Comparison for Coplanar Transfers Between Elliptic Orbits That Differ Only in Their Apsidal Orientation5.4 Hohmann Transfer
  • 5.5 The Bi-elliptic Transfer
  • 5.6 Restricted Three-Impulse Plane Change Maneuver for Circular Orbits
  • 5.7 General Three-Impulse Plane Change Maneuver for Circular Orbit
  • 5.8 Hohmann Transfer with Split-Plane Change
  • 5.9 Bi-elliptic Transfer with Split-Plane Change
  • 5.10 Transfer Between Coplanar Elliptic Orbits
  • References
  • Problems
  • Selected Solutions
  • Chapter 6. Complications to Impulsive Maneuvers6.1 N-Impulse Maneuvers
  • 6.2 Fixed-Impulse Transfers
  • 6.3 Finite-Duration Burns: Gravity Losses
  • 6.4 Very Low Thrust Transfers
  • References
  • Problems
  • Selected Solutions
  • Chapter 7. Relative Motion in Orbit
  • 7.1 Space Rendezvous
  • 7.2 Terminal Rendezvous
  • 7.3 Applications of Rendezvous Equations
  • 7.4 An Exact Analytical Solution for Two-Dimensional Relative Motion
  • 7.5 Optimal Multiple-Impulse Rendezvous
  • References
  • Problems
  • Selected Solutions

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