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Non-Coplanar Rendezvous in Near-Circular Orbit with the Use a Low Thrust Engine of a circular orbit.Simplified mathematical models of motion are used to solve this problem
Cylindrically symmetric wormholes WhC R e: The motion of test particles to the unstable circular orbit of radius uc. For D2>Dc2 there are two kinds of orbits: orbits of the first kind
Cylindrically symmetric wormholes WhC R e: The motion of test particles to the unstable circular orbit of radius uc. For D2>Dc2 there are two kinds of orbits: orbits of the first kind
Cylindrically symmetric wormholes WhC R e: The motion of test particles to the unstable circular orbit of radius uc. For D2>Dc2 there are two kinds of orbits: orbits of the first kind
Cylindrically symmetric wormholes WhC R e: The motion of test particles to the unstable circular orbit of radius uc. For D2>Dc2 there are two kinds of orbits: orbits of the first kind
Trajectories Derived from Periodic Orbits around the Lagrangian Point L1 and Lunar Swing-Bys: Application in Transfers to Near-Earth Asteroids periodic orbits around L1 are applied to a spacecraft in circular low Earth orbits in the same direction
Optimization of the finite-thrust trajectory in the vicinity of a circular orbit of the circular orbit. The fixed-time rendezvous missions are considered. The Hill-Clohessy-Wiltshire equations
Low-Energy Sub-Optimal Low-Thrust Trajectories to Libration Points and Halo-Orbits and calculating a low-thrust trajectory from an initial circular Earth orbit to the given point of this manifold
Stability analysis of circular geodesics in dyonic dilatonic black hole spacetimes, the innermost stable circular orbit (ISCO) is determined by reducing the problem to solving a fourth
Innermost stable circular orbit near dirty black holes in magnetic field and ultra-high-energy particle collisions© 2015, The Author(s). We consider the behavior of the innermost stable circular orbit (ISCO
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