Abstract. We investigate the arrangements of periodic orbits in a restricted, circular, 3-dimensional 3-body problem in which the primaries are the Sun and the Earth, and the massless body represents the Moon. By fixing the duration of the periodic orbits to a multiple of the synodic lunar month, we set up a numerical procedure that systematically finds all the periodic orbits of given duration, not only close to the current lunar orbit, i.e. at low eccentricity and low inclination, but also far from it. 1
In a prior study, a methodology was developed for computing approximate large displaced orbits in th...
As destinations of missions in both human and robotic spaceflight become more exotic, a foundational ...
Using the numerical solution in the plane restricted problem of three bodies, about 490 periodic orb...
In the framework of the restricted, circular, 3-dimensional 3-body problem Sun-Earth-Moon, Valsecchi...
This study employs the circular restricted three-body problem (CR3BP) as the dynamical framework, fo...
Solar sail technology offers new capabilities for the analysis and design of space missions. This ne...
In this paper, we have investigated a region of direct stable orbits around the Moon, whose stabilit...
The present work deals with a family of simply periodic orbits around the Moon in the rotating Earth...
This paper analyzes distant periodic orbits in the Earth-Moon system. Unstable periodic orbits in th...
This paper analyzes distant periodic orbits in the Earth-Moon system. Unstable periodic orbits in th...
This paper analyzes distant periodic orbits in the Earth-Moon system. Unstable periodic orbits in th...
This paper analyzes distant periodic orbits in the Earth-Moon system. Unstable periodic orbits in th...
The renewed interest in Lunar exploration prompts a need to better understand the dynamics of spacec...
Solar sail technology offer new capabilities for the analysis and design of space missions. This new...
Classification scheme for symmetric periodic orbits in restricted three body problem with two dimens...
In a prior study, a methodology was developed for computing approximate large displaced orbits in th...
As destinations of missions in both human and robotic spaceflight become more exotic, a foundational ...
Using the numerical solution in the plane restricted problem of three bodies, about 490 periodic orb...
In the framework of the restricted, circular, 3-dimensional 3-body problem Sun-Earth-Moon, Valsecchi...
This study employs the circular restricted three-body problem (CR3BP) as the dynamical framework, fo...
Solar sail technology offers new capabilities for the analysis and design of space missions. This ne...
In this paper, we have investigated a region of direct stable orbits around the Moon, whose stabilit...
The present work deals with a family of simply periodic orbits around the Moon in the rotating Earth...
This paper analyzes distant periodic orbits in the Earth-Moon system. Unstable periodic orbits in th...
This paper analyzes distant periodic orbits in the Earth-Moon system. Unstable periodic orbits in th...
This paper analyzes distant periodic orbits in the Earth-Moon system. Unstable periodic orbits in th...
This paper analyzes distant periodic orbits in the Earth-Moon system. Unstable periodic orbits in th...
The renewed interest in Lunar exploration prompts a need to better understand the dynamics of spacec...
Solar sail technology offer new capabilities for the analysis and design of space missions. This new...
Classification scheme for symmetric periodic orbits in restricted three body problem with two dimens...
In a prior study, a methodology was developed for computing approximate large displaced orbits in th...
As destinations of missions in both human and robotic spaceflight become more exotic, a foundational ...
Using the numerical solution in the plane restricted problem of three bodies, about 490 periodic orb...