Add to ORKGWe describe how to determine transfers between libration point orbits and either the surface of the Moon or a Low Earth Orbit within the Circular Restricted Three – Body Problem (CR3BP) assumptions. Moreover, we explain how to refine such trajectories to ones verifing more comprehensive equations of motion. We are interested in seeing how the geometry of the nominal target orbits and of the associated stable manifolds drives the connections and also how much reliable the CR3BP is. The main tools we take advantage of are the Lindstedt–Poincaré semi-analytical method, differential correction procedures and an optimizer
Consider the design of transfer trajectories to the vicinity of the Sun-Earth collinear libration po...
A search for low Δ V Earth-to-Moon trajectories has been initiated. Numerical integration of the equ...
In the framework of the planar CR3BP for mass parameter mu=0.0121505, corresponding to the Earth-Moo...
This work deals with the design of transfers connecting LEOs with halo orbits around libration point...
An increasing interest in lunar exploration calls for low-cost techniques of reaching the Moon. Ball...
An increasing interest in lunar exploration calls for low-cost techniques of reaching the Moon. Ball...
The planar, circular, restricted three-body problem predicts the existence of periodic orbits around...
This paper is devoted to the study of the transfer problem from a libration point orbit of the Earth...
The dynamics of the circular restricted three-body Earth-Moon-particle problem predicts the existenc...
The planar, circular, restricted three-body problem predicts the existence of periodic orbits around...
This paper is devoted to the study of the transfer problem from a libration point orbit of the Earth...
A renewed interest in the Moon over the last decade has created a need for robust mission design alg...
This paper is devoted to the study of the transfer problem from a libration point orbit of the Earth...
This paper presents two ways to transfer a spacecraft to distant periodic orbits in the Earth–Moon s...
Abstract: Trajectories connecting LEOs with halos around libration points of the Earth– Moon CRTBP a...
Consider the design of transfer trajectories to the vicinity of the Sun-Earth collinear libration po...
A search for low Δ V Earth-to-Moon trajectories has been initiated. Numerical integration of the equ...
In the framework of the planar CR3BP for mass parameter mu=0.0121505, corresponding to the Earth-Moo...
This work deals with the design of transfers connecting LEOs with halo orbits around libration point...
An increasing interest in lunar exploration calls for low-cost techniques of reaching the Moon. Ball...
An increasing interest in lunar exploration calls for low-cost techniques of reaching the Moon. Ball...
The planar, circular, restricted three-body problem predicts the existence of periodic orbits around...
This paper is devoted to the study of the transfer problem from a libration point orbit of the Earth...
The dynamics of the circular restricted three-body Earth-Moon-particle problem predicts the existenc...
The planar, circular, restricted three-body problem predicts the existence of periodic orbits around...
This paper is devoted to the study of the transfer problem from a libration point orbit of the Earth...
A renewed interest in the Moon over the last decade has created a need for robust mission design alg...
This paper is devoted to the study of the transfer problem from a libration point orbit of the Earth...
This paper presents two ways to transfer a spacecraft to distant periodic orbits in the Earth–Moon s...
Abstract: Trajectories connecting LEOs with halos around libration points of the Earth– Moon CRTBP a...
Consider the design of transfer trajectories to the vicinity of the Sun-Earth collinear libration po...
A search for low Δ V Earth-to-Moon trajectories has been initiated. Numerical integration of the equ...
In the framework of the planar CR3BP for mass parameter mu=0.0121505, corresponding to the Earth-Moo...