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Mittleman, D. and Jezwski, D. (1982) An Analytic Solution to the Classical Two-Body Problem with Drag. Celestial Mechanics and Dynamical Astronomy, 28, 401-413.
http://dx.doi.org/10.1007/BF01372122

has been cited by the following article:

• TITLE: Use of an Energy-Like Integral to Study the Motion of an Axi-Symmetric Satellite under Drag and Radiation Pressure

  AUTHORS: Ahmed Mostafa

  KEYWORDS: Artificial Satellite, Drag Effect, Radiation Pressure

  JOURNAL NAME: International Journal of Astronomy and Astrophysics, Vol.5 No.3, September 1, 2015

  ABSTRACT: The axi-symmetric satellite problem including radiation pressure and drag is treated. The equations of motion of the satellite are derived. An energy-like is given for a general drag force function of the polar angle θ, and then it is used to find a relation for the orbit equation of the satellite with initial conditions satisfying the vanishing of arbitrarily choosing higher derivatives of the velocity.