High-order solutions around triangular libration points in the elliptic restricted three-body problem and applications to low energy transfers
From MaRDI portal
Publication:2300259
DOI10.1016/j.cnsns.2014.01.019OpenAlexW2084283458MaRDI QIDQ2300259
Publication date: 27 February 2020
Published in: Communications in Nonlinear Science and Numerical Simulation (Search for Journal in Brave)
Full work available at URL: https://doi.org/10.1016/j.cnsns.2014.01.019
triangular libration pointsLindstedt-Poincaré methodseries expansionselliptic restricted three-body problemlow-thrust low energy transfertwo-impulse low energy transfer
Related Items (9)
Analytical study on the motions around equilibrium points of restricted four-body problem ⋮ Fast numerical approximation of invariant manifolds in the circular restricted three-body problem ⋮ Low-energy transfers to cislunar periodic orbits visiting triangular libration points ⋮ Higher order approximation to the Hill problem dynamics about the libration points ⋮ Single impulsive transfer to the Earth-Moon triangular point L\(_4\) in a bicircular model ⋮ Semianalytical solutions of relative motions with applications to periodic orbits about a nominal circular orbit ⋮ Transfers between libration point orbits of Sun-Earth and Earth-Moon systems by using invariant manifolds ⋮ Polynomial expansions of single-mode motions around equilibrium points in the circular restricted three-body problem ⋮ Explicit solution and resonance dynamics around triangular libration points of the planar elliptic restricted three-body problem
Cites Work
- Unnamed Item
- Unnamed Item
- On quasi-periodic motions around the collinear libration points in the real Earth-Moon system
- Earth-Mars transfers with ballistic escape and low-thrust capture
- Efficient invariant-manifold, low-thrust planar trajectories to the Moon
- Intersecting invariant manifolds in spatial restricted three-body problems: design and optimization of Earth-to-halo transfers in the Sun-Earth-Moon scenario
- Penalty function approach for the mixed discrete nonlinear problems by particle swarm optimization
- Earth-Mars halo to halo low thrust manifold transfers
- Low-energy, low-thrust transfers to the Moon
- On quasi-periodic motions around the triangular libration points of the real Earth-Moon system
- Leaving the moon by means of invariant manifolds of libration point orbits
- High-order analytical solutions of Hill's equations
- On target for Venus -- set oriented computation of energy efficient low thrust trajectories
- Dynamics in the center manifold of the collinear points of the restricted three-body problem
- Computation of low energy Earth-to-Moon transfers with moderate flight time
- Dynamics and Mission Design Near Libration Points
- An Introduction to Celestial Mechanics
- Conversion of Optimal Control Problems into Parameter Optimization Problems
- Survey of Numerical Methods for Trajectory Optimization
- Three-dimensional periodic orbits about the triangular equilibrium points of the restricted problem of three bodies
- Analytic construction of periodic orbits about the collinear points
- Traveling Between the Lagrange Points and the Moon
- Dynamics and Mission Design Near Libration Points
- High-order expansions of invariant manifolds of libration point orbits with applications to mission design
- Quasi-periodic orbits about the translunar libration point
- Low energy transfer to the Moon
This page was built for publication: High-order solutions around triangular libration points in the elliptic restricted three-body problem and applications to low energy transfers