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Construction of an optimal transition orbit with regard to the drag of the atmosphere, nonsphericity of the Earth, and perturbations of Moon and Sun. (Russian. English summary) Zbl 0628.70026

Analytical construction of an optimal two-impulse transfer in the equatorial plane of an axisymmetrical planet between the elliptic orbits of small eccentricities is given while taking into account secular perturbations from the atmospheric drag as well as from the Moon and the Sun.

MSC:

70M20 Orbital mechanics
70Q05 Control of mechanical systems
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