内容

目次

Preface; 1. The Fundamental Classic Analysis of Edelbaum, Sackett and Malchow, with Additional Detailed Derivations and Extensions; 2. The Analysis of the Six-Element Formulation; 3. Optimal Low-Thrust Rendezvous Using Equinoctial Orbit Elements; 4. Optimal Low-Thrust Transfer Using Variable Bounded Thrust; 5. Minimum-Time Low-Thrust Rendezvous and Transfer Using Epoch Mean Longitude Formulation; 6. Trajectory Optimization Using Eccentric Longitude Formulation; 7. Low-Thrust Trajectory Optimization Based On Epoch Eccentric Longitude Formulation; 8. Mechanics of Trajectory Optimization Using Nonsingular Variational Equations in Polar Coordinates; 9. Trajectory Optimization Using Nonsingular Orbital Elements and True Longitude; 10. The Treatment of the Earth Oblateness Effect in Trajectory Optimization in Equinoctial Coordinates; 11. Minimum-Time Constant Acceleration Orbit Transfer with First-Order Oblateness Effect; 12. The Streamlined and Complete Set of the Nonsingular J2-Perturbed Dynamic and Adjoint Equations for Trajectory Optimization in Terms of Eccentric Longitude; 13. The Inclusion of the Higher Order Harmonics in the Modeling of Optimal Low-Thrust Orbit Transfer; 14. Analytic Expansions of Luni-Solar Gravity Perturbations along Rotating Axes for Trajectory Optimization: Part 1: The Dynamic System; 15. Analytic Expansions of Luni-Solar Gravity Perturbations along Rotating Axes for Trajectory Optimization: Part 2: The Multipliers System and Simulations; 16. Fourth Order Expansions of the Luni-Solar Gravity Perturbations along Rotating Axes for Trajectory Optimization; Index.