Add to ORKGIn a prior study, a methodology was developed for computing approximate large displaced orbits in the Earth-Moon circular restricted three-body problem (CRTBP)by the Moon-Sail two-body problem. It was found that far from the L1 and L2 points, the approximate two-body analysis for large accelerations matches well with the dynamics of displaced orbits in relation to the three-body problem. In the present study, the linear stability characteristics of the families of approximate periodic orbits are investigated
The Earth-Moon system is nowadays attracting more and more interest as a well suited location for ne...
The Earth-Moon system is nowadays attracting more and more interest as a well suited location for ne...
The Earth-Moon system is nowadays attracting more and more interest as a well suited location for ne...
In a prior study, a methodology was developed for computing approximate large displaced orbits in th...
This work deals with the structure of the lunar Weak Stability Boundaries (WSB) in the framework of ...
The present work deals with a family of simply periodic orbits around the Moon in the rotating Earth...
Abstract. We investigate the arrangements of periodic orbits in a restricted, circular, 3-dimensiona...
In this paper, we have investigated a region of direct stable orbits around the Moon, whose stabilit...
Previous studies for small formation flying dynamics about triangular libration points have determin...
Previous studies for small formation flying dynamics about triangular libration points have determin...
Solar sailing and solar electric technology provide alternative forms of spacecraft propulsion. Thes...
Previous studies for small formation flying dynamics about triangular libration points have determin...
The Three Body Problem (3BP) has been one of the main celestial mechanics problems in the past few c...
The Earth-Moon system is nowadays attracting more and more interest as a well suited location for ne...
The Earth-Moon system is nowadays attracting more and more interest as a well suited location for ne...
The Earth-Moon system is nowadays attracting more and more interest as a well suited location for ne...
The Earth-Moon system is nowadays attracting more and more interest as a well suited location for ne...
The Earth-Moon system is nowadays attracting more and more interest as a well suited location for ne...
In a prior study, a methodology was developed for computing approximate large displaced orbits in th...
This work deals with the structure of the lunar Weak Stability Boundaries (WSB) in the framework of ...
The present work deals with a family of simply periodic orbits around the Moon in the rotating Earth...
Abstract. We investigate the arrangements of periodic orbits in a restricted, circular, 3-dimensiona...
In this paper, we have investigated a region of direct stable orbits around the Moon, whose stabilit...
Previous studies for small formation flying dynamics about triangular libration points have determin...
Previous studies for small formation flying dynamics about triangular libration points have determin...
Solar sailing and solar electric technology provide alternative forms of spacecraft propulsion. Thes...
Previous studies for small formation flying dynamics about triangular libration points have determin...
The Three Body Problem (3BP) has been one of the main celestial mechanics problems in the past few c...
The Earth-Moon system is nowadays attracting more and more interest as a well suited location for ne...
The Earth-Moon system is nowadays attracting more and more interest as a well suited location for ne...
The Earth-Moon system is nowadays attracting more and more interest as a well suited location for ne...
The Earth-Moon system is nowadays attracting more and more interest as a well suited location for ne...
The Earth-Moon system is nowadays attracting more and more interest as a well suited location for ne...