低能飛行 : 太空飛行器軌道動力學與任務軌道設計

圖書簡介

The book focuses on the orbital dynamics and mission trajectory (transfer or target trajectory) design of low-energy flight in the context of modern astrodynamics. It investigates various topics that either offer new methods for solving classical problems or address emerging problems that have yet to be studied, including low-thrust transfer trajectory design using the virtual gravity field method; transfer in the three body system using invariant manifolds; formation flying under space-borne artificial magnetic fields; and the orbital dynamics of highly irregular asteroids. It also features an extensive study of the orbital dynamics in the vicinity of contact binary asteroids, the third-order analytical solution of orbital motion in the vicinity of the non-collinear equilibrium point.

圖書目錄

Preface
Chapter 1 Introduction
Chapter 2 Continuous Low Thrust Trajectory Design and Optimization
Chapter 3 Transfer Between Libration Point Orbits and Lunar Orbits in Earth-Moon System
Chapter 4 Lorentz Force Formation Flying in the Earth-Moon System
Chapter 5 1∶1 Ground-Track Resonance in a 4th Degree and Order Gravitational Field
Chapter 6 Orbital Dynamics in the Vicinity of Contact Binary Asteroid Systems
Appendix A The Primary Zonal and Tesseral Terms Contributing to the 1∶1 Resonance
Appendix B The Un-normalized Spherical Harmonic Coefficients to Degree and Order 4
Appendix C The Location of EPs and Resonance Width
Appendix D The Second Derivatives of the Potential at the Eps Located at (x<sub>0</sub>, y<sub>0</sub>, 0)
Appendix E The First and Second Derivatives of the ξ Component

低能飛行 : 太空飛行器軌道動力學與任務軌道設計

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