Construction of an algorithm for taking into account atmospheric drag when investigating the motion of an artificial earth satellite

Details Construction of an algorithm for taking into account atmospheric drag when investigating the motion of an artificial earth satellite Construction of an algorithm for taking into account atmospheric drag when investigating the motion of an artificial earth satellite

Apr 1989

adsabs.harvard.edu/cgi-bin/nph-data_query?bibcode=1989azh....66..404s&link_type=abstract

Astronomicheskii Zhurnal (ISSN 0004-6299), vol. 66, Mar.-Apr. 1989, p. 404-411. In Russian.

Astronomy and Astrophysics

Astronomy

Aerodynamic Drag, Artificial Satellites, Earth Atmosphere, Satellite Drag, Algorithms, Perturbation Theory

Scientific paper

An analytical theory for taking into account perturbations due to
atmospheric drag in investigations of satellite motion is developed. The
theory is based on an asymmetric variant of the Euler intermediate
orbit. The expansion of components of perturbing acceleration due to the
drag of a satellite in a stationary rotating atmosphere is presented.

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