| Preface |
| Chapter 1 TWO-BODY ORBITAL MECHANICS |
| 1.1 Historical Background and Basic Laws |
| 1.2 The N-Body Problem |
| 1.3 The Two-Body Problem |
| 1.4 Constants of the Motion |
| 1.5 The Trajectory Equation |
| 1.6 Relating E and h to the Geometry of an Orbit |
| 1.7 The Elliptical Orbit |
| 1.8 The Circular Orbit |
| 1.9 The Parabolic Orbit |
| 1.10 The Hyperbolic Orbit |
| 1.11 Canonical Units |
| Exercises |
| List of References |
| Chapter 2 ORBIT DETERMINATION FROM OBSERVATIONS |
| 2.1 Historical Background |
| 2.2 Coordinate Systems |
| 2.3 Classical Orbital Elements |
| 2.4 Determining the Orbital Elements from r and v |
| 2.5 Determining r and v from the Orbital Elements |
| 2.6 Coordinate Transformations |
| 2.7 Orbit Determination from a Single Radar Observation |
| 2.8 SEZ to IJK Transformation Using an Ellipsoid Earth Model |
| 2.9 The Measurement of Time |
| 2.10 Orbit Determination from Three Position Vectors |
| 2.11 Orbit Determination from Optical Sightings |
| 2.12 Improving a Preliminary Orbit by Differential Correction |
| 2.13 Space Survelliance |
| 2.14 Type and Location of Sensors |
| 2.15 Ground Track of a Satellite |
| Exercises |
| List of References |
| Chapter 3 BASIC ORBITAL MANEUVERS |
| 3.1 Low Altitiude Earth Orbits |
| 3.2 High Altitude Earth Orbits |
| 3.3 In-Plane Orbit Changes |
| 3.4 Out-Of-Plane Orbit Changes |
| Exercises |
| List of References |
| Chapter 4 POSITION AND VELOCITY AS A FUNCTION OF TIME |
| 4.1 Historical Background |
| 4.2 Time-of-Flight as a Function of Eccentric Anomaly |
| 4.3 A Universal Fomulation for Time-of-Flight |
| 4.4 The Prediction Problem |
| 4.5 Implementing the Universal Variable Formulation |
| 4.6 Classical Formulations of the Kepler Problem |
| Exercises |
| List of References |
| Chapter 5 ORBIT DETERMINATION FROM TWO POSITIONS AND TIME |
| 5.1 Historical Background |
| 5.2 The Gauss Problem - General Methods of Solution |
| 5.3 Solution of the Gauss Problem via Universal Variables |
| 5.4 The p-Iteration Method |
| 5.5 The Gauss Problem Using the f and g Series |
| 5.6 The Original Gauss Method |
| 5.7 Practical Applications of the Gauss Problem - Intercept and Rendezvous |
| 5.8 Determination of Orbit from Sighting Directions at Station |
| Exercises |
| List of References |
| Chapter 6 BALLISTIC MISSILE TRAJECTORIES |
| 6.1 Historical Background |
| 6.2 The General Ballistic Missile Problem |
| 6.3 Effect of Launching Errors on Range |
| 6.4 The Effect of Earth Rot |
| Exercises |
| List of References |
| Chapter 7 LUNAR TRAJECTORIES |
| 7.1 Historical Background |
| 7.2 The Earth-Moon System |
| 7.3 Simple Earth-Moon Trajectories |
| 7.4 The Patched-Conic Approximation |
| 7.5 Non-Coplanar Lunar Trajectories |
| Exercises |
| List of References |
| Chapter 8 INTERPLANETARY TRAJECTORIES |
| 8.1 Historical Background |
| 8.2 The Solar System |
| 8.3 The Patched-Conic Approximation |
| 8.4 Non-Coplanar Interplanetary Trajectories |
| Exercises |
| List of References |
| Chapter 9 PERTURBATIONS |
| 9.1 Introduction and Historical Background |
| 9.2 Cowell's Method |
| 9.3 Encke's Method |
| 9.4 Variation of Parameters or Elements |
| 9.5 Comments on Integration Schemes and Errors |
| 9.6 Numerical Integration Methods |
| 9.7 Analytic Formulation of Perturbative Accelerations |
| Exercises |
| List of References |
| Appendix A Astrodynamic Constants |
| Appendix B Miscellaneous Constants and Conversions |
| Appendix C Vector Review |
| Appendix D Suggested Projects |
| Index |