Operational requirements and the geometry of a station-keeping maneuver

Details Operational requirements and the geometry of a station-keeping maneuver Operational requirements and the geometry of a station-keeping maneuver

Nov 1977

adsabs.harvard.edu/cgi-bin/nph-data_query?bibcode=1977cemec..16..315e&link_type=abstract

Celestial Mechanics, vol. 16, Nov. 1977, p. 315-342.

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2

Astrodynamics, Orbital Maneuvers, Satellite Orbits, Stationkeeping, Circular Orbits, Differential Equations, Equations Of Motion, Inertia, Operational Problems, Orbital Mechanics, Thrust

Scientific paper

A linear solution is applied to the problem of orbital dynamics as it pertains to the station-keeping of a satellite. Attention is given to the retention of a relative motion sub-orbit, whose parameters are expressed in a dimensionless format so that the results apply to other reference orbits. Both initial relative motion states and thrusting conditions are examined, especially in terms of their application to an inertially aligned frame of reference (as opposed to a rotating one).

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