Dynamical structures in a low-thrust, multi-body model with applications to trajectory design
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Publication:2005605
DOI10.1007/S10569-019-9891-7zbMath1451.70018OpenAlexW2918780870MaRDI QIDQ2005605
Kathleen C. Howell, Andrew D. Cox, David C. Folta
Publication date: 8 October 2020
Published in: Celestial Mechanics and Dynamical Astronomy (Search for Journal in Brave)
Full work available at URL: https://doi.org/10.1007/s10569-019-9891-7
periodic orbitsequilibrium solutionslow-thrustforbidden regionsspacecraft trajectory designmulti-body dynamical systems
Related Items (2)
Linking low- to high-energy dynamics of invariant manifolds, transit orbits, and singular collision orbits in the planar circular restricted three-body problem ⋮ Transit and capture in the planar three-body problem leveraging low-thrust invariant manifolds
Cites Work
- Earth-Mars transfers with ballistic escape and low-thrust capture
- Efficient invariant-manifold, low-thrust planar trajectories to the Moon
- Numerical study of the geometry of the phase space of the Augmented Hill Three-Body problem
- Dynamics and Mission Design Near Libration Points
- Heteroclinic connections between periodic orbits and resonance transitions in celestial mechanics
- Connecting orbits and invariant manifolds in the spatial restricted three-body problem
- Low Energy Transit Orbits in the Restricted Three-Body Problems
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