Book contents
- Frontmatter
- Dedication
- Contents
- Preface
- Nomenclature
- 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: The Dynamic System
- 15 Analytic Expansions of Luni-Solar Gravity Perturbations Along Rotating Axes for Trajectory Optimization: The Multipliers System and Simulations
- 16 Fourth-Order Expansions of the Luni-Solar Gravity Perturbations along Rotating Axes for Trajectory Optimization
- Index
12 - The Streamlined and Complete Set of the Nonsingular J2-Perturbed Dynamic and Adjoint Equations for Trajectory Optimization in Terms of Eccentric Longitude
Published online by Cambridge University Press: 04 August 2018
Book contents
- Frontmatter
- Dedication
- Contents
- Preface
- Nomenclature
- 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: The Dynamic System
- 15 Analytic Expansions of Luni-Solar Gravity Perturbations Along Rotating Axes for Trajectory Optimization: The Multipliers System and Simulations
- 16 Fourth-Order Expansions of the Luni-Solar Gravity Perturbations along Rotating Axes for Trajectory Optimization
- Index
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- Applied Nonsingular AstrodynamicsOptimal Low-Thrust Orbit Transfer, pp. 304 - 327Publisher: Cambridge University PressPrint publication year: 2018