Chapter 1. The Second-Order Analytic Approximation to the Solution of the Euler-Hill Equations of Relative Motion.- Chapter 2. Analytic Solutions for the Perturbed Motion of a Spacecraft in Near-Circular Orbit, Under the Influence of the J2 and J3 Earth Zonal Harmonics, in Rotating and Inertial Cartesian Reference Frames.- Chapter 3. Analytic Solutions for the Perturbed Motion of a Spacecraft in Near-Circular Orbit, Under the Influence of the Luni-Solar Gravity, in Rotating and Inertial Cartesian Reference Frames.- Chapter 4. Effect of Luni-Solar Gravity Perturbations on a Near-Circular Orbit: Third-Body Orbit Eccentricity Considerations.- Chapter 5. Effect of Atmospheric Drag Perturbation on Circular Orbits: Atmosphere Rotation Considerations.- Chapter 6. Analytic Solution of Terminal Rendezvous in Near-Circular Orbit Around the Oblate Earth: The Computation of the Starting Guess for Iterations.- Chapter 7. Techniques of Accurate Analytic Terminal Rendezvous in Near-Circular Orbit.- Chapter 8. Coplanar Two-Impulse Rendezvous in General Elliptic Orbit with Drag.- Chapter 9. The Analysis of the Relative Motion in General Elliptic Orbit With Respect to a Dragging and Precessing Coordinate Frame.- Chapter 10. The Algorithm of the Two-Impulse Time-Fixed Noncoplanar Rendezvous with Drag and Oblateness Effects.- Chapter 11. The Analysis and Implementation of In-Plane Stationkeeping of Continuously Perturbed Walker Constellations.- Chapter 12. The Mathematical Models of the Jet Propulsion Laboratory (JPL) Artificial Satellite Analysis Program (ASAP)
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