Investigation of the controlled coplanar relative motion of space vehicles for a constant angular velocity along the line of sight

Details Investigation of the controlled coplanar relative motion of space vehicles for a constant angular velocity along the line of sight Investigation of the controlled coplanar relative motion of space vehicles for a constant angular velocity along the line of sight

Sep 1974

adsabs.harvard.edu/cgi-bin/nph-data_query?bibcode=1974kosis..12..691i&link_type=abstract

Kosmicheskie Issledovaniia, vol. 12, Sept.-Oct. 1974, p. 691-700. In Russian.

Physics

Circular Orbits, Orbital Rendezvous, Rendezvous Guidance, Space Stations, Spacecraft Guidance, Trajectory Control, Angular Velocity, Coplanarity, Fuel Consumption, Orbital Velocity, Spacecraft Maneuvers, Spacecraft Motion

Scientific paper

The phase space of states of the relative motion of a spacecraft in the
proximity of an orbital station in circular orbit is examined. Possible
types of relative motion trajectories are determined, using control
methods analogous to inertial and orbital guidance techniques. The power
requirements of the control methods are evaluated.

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