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Satellite in Keplerian Orbit

2014
The position of a body orbiting in a Keplerian motion is defined by the 6 Keplerian elements. From now on, we shall be mainly concerned with the periodic motion of a body, the artificial satellite, in the gravitational field of the Earth.
exaly   +2 more sources

Keplerian Representation of a Non-Keplerian Orbit

Journal of Guidance and Control, 1980
The properties of a mean reference orbit are developed through the introduction of an augmented radial potential proportional to c/r2. The arbitrary constant c is chosen to satisfy the perturbed energy level over an oblate Earth. This produces a mean orbit with not only the correct first order anomalistic period, but one which is also functionally ...
openaire   +1 more source

Families of Keplerian orbits

European Journal of Physics, 2003
Summary: Various properties of Keplerian orbits traced by satellites that are launched from the same spatial point with different initial velocities are discussed. Two families of elliptical orbits are investigated, namely the sets of orbits produced by a common direction but different magnitudes of the initial velocities, and by a common magnitude but
openaire   +2 more sources

Principal Periodic Orbits of the Keplerian Dumbbell System

SIAM Journal on Applied Dynamical Systems, 2020
zbMATH Open Web Interface contents unavailable due to conflicting licenses.
Rui Dilão, Manuel Murteira
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Non-Keplerian orbits for electric sails

Celestial Mechanics and Dynamical Astronomy, 2009
zbMATH Open Web Interface contents unavailable due to conflicting licenses.
MENGALI, GIOVANNI   +1 more
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On Feynman’s analysis of the geometry of Keplerian orbits

American Journal of Physics, 2003
A geometrical construction, introduced by Maxwell and Feynman to demonstrate that closed Keplerian orbits are elliptical, is adapted to show that open Keplerian orbits are hyperbolic or parabolic.
Kowen, Michael, Mathur, H.
openaire   +1 more source

Satellite transfers between Keplerian orbits

Celestial Mechanics and Dynamical Astronomy, 2022
zbMATH Open Web Interface contents unavailable due to conflicting licenses.
Rui Dilão   +2 more
openaire   +2 more sources

Keplerian Orbit and Satellite skCUBE

2019 New Trends in Aviation Development (NTAD), 2019
This paper describes the basic concepts for determining the cosmic objects position and motion according to the Kepler's Laws and Newton's law of Universal Gravitation. In addition, the paper also includes an algorithm to compute the (miniature) satellites orbit. The algorithm input data was received from two-line elements (TLE) record.
P. Szabo   +3 more
openaire   +1 more source

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