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Satellites’ orbits in the Sun–Earth–Moon system
There is a large set of papers and monographs which consider the restricted three-body problem and apply the results to the orbits of satellites or...
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Features of Space Debris Migration in the Earth–Moon System
Abstract —The possibility of capturing and releasing cosmic masses is considered within the framework of a plane hyperbolic three-body problem, as...
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Growth of the Moon Due To Bodies Ejected from the Earth
Abstract —The evolution of the orbits of bodies ejected from the Earth has been studied at the stage of its accumulation and early evolution after...
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Low-energy Earth–Moon transfers via Theory of Functional Connections and homotopy
Numerous missions leverage the weak stability boundary in the Earth–Moon–Sun system to achieve a safe and cost-effective access to the lunar...
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Analysis of the Effect of Earth’s Equatorial Ellipticity on the Existence and Stability of the Lagrangian Points in the Earth–Moon–Sun System
AbstractWe have investigated existence of Lagrangian points and analyzed stability in the Earth–Moon–Sun system including the effect of Earth’s...
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Dynamics around the Earth–Moon triangular points in the Hill restricted 4-body problem
This paper investigates the motion of a small particle moving near the triangular points of the Earth–Moon system. The dynamics are modeled in the...
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On the Probability of Capturing Preplanetary Bodies into the Protolunar Swarm During the Formation of the Earth−Moon System
AbstractThe probability of capturing preplanetary bodies into the protolunar swarm is considered in the dependence on the distance of a collision...
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On optimal three-impulse Earth–Moon transfers in a four-body model
Within the emerging age of lunar exploration, optimizing transfer trajectories is a fundamental measure toward achieving more economical and...
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Model predictive control-based coupled orbit-attitude control for solar sail formation flying in the Earth-Moon system
This paper investigates the problem of coupled orbit-attitude control for solar sail formation flying where the leader follows a solar-sail resonant...
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A Method for Calculating the Trajectory of a Single-Impulse Flight to a Halo Orbit around the L2 Libration Point of the Earth–Moon System
AbstractThe problem of calculation of low-energy impulse trajectories to halo orbits in the vicinity of the L 2 point of the Earth–Moon system is...
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The Earth, the Moon, Mercury, Saturn and Its Rings, and Asteroids
The planets Earth and Saturn have dense atmosphere and strong intrinsic magnetic field and hence a sturdy magnetosphere. Therefore, both of these...
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Two-impulse transfer to multi-revolution halo orbits in the Earth–Moon elliptic restricted three body problem framework
For the design of transfer trajectories in the Earth–Moon system, the manifolds theory is popularly used in the existing literature. Because the...
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The Earth–Moon System
Thus far, we have methodically developed and presented a set of tools that allows the reader to formulate a perturbation problem in a straightforward...
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The Earth, the Moon, Mercury, Saturn and Its Rings, and Asteroids
The planets Earth and Saturn have dense atmosphere and strong intrinsic magnetic field and hence a sturdy magnetosphere. Therefore, both of these...
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The Earth, the Moon, Mercury, Saturn and Its Rings, and Asteroids
The planets Earth and Saturn have dense atmosphere and strong intrinsic magnetic field and hence a sturdy magnetosphere. Therefore, both of these...
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Analysis of Resonant Curve in a Synchronous Satellite under the Gravitational Effect of the Sun, the Moon, and the Earth Including Its Oblateness using Poincare Section
AbstractIn this paper, we have studied the effect of oblateness of the Earth on the resonant curve in synchronous satellite under the gravitational...
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3D stable and weakly unstable periodic orbits around the Earth near the retrograde co-orbital resonance with the Moon
Stable or weakly unstable orbits in cislunar space are attractive as potential locations that natural objects including dust particles may be...
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