Quasi-analytical solutions for the dynamics of a class of tethered satellites with Danby's aerodynamical drag

Details Quasi-analytical solutions for the dynamics of a class of tethered satellites with Danby's aerodynamical drag Quasi-analytical solutions for the dynamics of a class of tethered satellites with Danby's aerodynamical drag

Dec 1985

adsabs.harvard.edu/cgi-bin/nph-data_query?bibcode=1985cemec..37..371b&link_type=abstract

Celestial Mechanics (ISSN 0008-8714), vol. 37, Dec. 1985, p. 371-385. Research supported by the Ministero della Pubblica Istruzi

Astronomy and Astrophysics

Astronomy

Aerodynamic Drag, Astrodynamics, Satellite Drag, Tethered Satellites, Anomalies, Mathematical Models, Quadratures

Scientific paper

An analytic solution, in terms of expansion of a small parameter, for
the classical two-body tethered satellite with a specific drag model
(Danby, 1962) is obtained. The time of flight as well as the solution
regarding the state variable of the system are expressed in terms of
quadratures of the anomaly.

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