Qualitative study of the motion of a spacecraft under constant radial acceleration

Details Qualitative study of the motion of a spacecraft under constant radial acceleration Qualitative study of the motion of a spacecraft under constant radial acceleration

Mar 1982

adsabs.harvard.edu/cgi-bin/nph-data_query?bibcode=1982kosis..20..191i&link_type=abstract

Kosmicheskie Issledovaniia, vol. 20, Mar.-Apr. 1982, p. 191-195. In Russian.

Physics

Acceleration (Physics), Radial Velocity, Spacecraft Motion, Trajectory Analysis, Dynamic Characteristics, Geosynchronous Orbits, Low Thrust Propulsion, Orbital Maneuvers

Scientific paper

The qualitative theory of dynamic systems of Andronov et al. (1966, 1967) is used to study the trajectories of the controlled motion of a spacecraft under constant radial acceleration. All possible types of trajectories of this class are determined, and attention is given to the application of the qualitative results to the synthesis of various orbital maneuver schemes with low radial thrust.

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