Investigation of the relative motion of two tethered bodies with regulated tether length

Details Investigation of the relative motion of two tethered bodies with regulated tether length Investigation of the relative motion of two tethered bodies with regulated tether length

Jul 1986

adsabs.harvard.edu/cgi-bin/nph-data_query?bibcode=1986kosis..24..544i&link_type=abstract

Kosmicheskie Issledovaniia (ISSN 0023-4206), vol. 24, July-Aug. 1986, p. 544-552. In Russian.

Mathematics

Elliptical Orbits, Orbit Perturbation, Spacecraft Motion, Tethered Satellites, Two Body Problem

Scientific paper

The qualitative theory of dynamic systems is used to study all possible types of trajectories of the relative motion of two tethered satellites for two sufficiently general laws for the regulation of tether length. Mathematical modeling is used to assess the applicability of the qualitative results to the analysis of the relative motion of the tethered bodies with allowance for the effect of a number of perturbing factors. Simulation results are presented for spacecraft motion in an elliptical orbit.

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