Evolution of the rotational motion of two tethered bodies in orbit

Details Evolution of the rotational motion of two tethered bodies in orbit Evolution of the rotational motion of two tethered bodies in orbit

Sep 1990

adsabs.harvard.edu/cgi-bin/nph-data_query?bibcode=1990kosis..28..692a&link_type=abstract

Kosmicheskie Issledovaniia (ISSN 0023-4206), vol. 28, Sept.-Oct. 1990, p. 692-701. In Russian.

Computer Science

Satellite Rotation, Spacecraft Orbits, Tethered Satellites, Two Body Problem, Aerodynamic Forces, Approximation, Circular Orbits, Kinematic Equations

Scientific paper

The kinematic evolution of two tethered point masses moving in an unperturbed Keplerian orbit is analyzed. It is shown that, in the first approximation, the motion of the kinetic-moment vector with respect to the motion of the system does not depend on oscillations along the tether. It is also demonstrated that the effect of the dissipative component of aerodynamic forces in circular orbit differs qualitatively from the effect described previously for a symmetrical rigid body.

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