Guidance of space vehicles in the case of a variable angular velocity of the line of sight

Details Guidance of space vehicles in the case of a variable angular velocity of the line of sight Guidance of space vehicles in the case of a variable angular velocity of the line of sight

Sep 1978

adsabs.harvard.edu/cgi-bin/nph-data_query?bibcode=1978kosis..16..659i&link_type=abstract

Kosmicheskie Issledovaniia, vol. 16, Sept.-Oct. 1978, p. 659-664. In Russian.

Physics

Angular Velocity, Optimal Control, Spacecraft Docking, Spacecraft Guidance, Trajectory Optimization, Control Theory, Equations Of Motion, Orbital Maneuvers, Rendezvous Trajectories

Scientific paper

In the present paper, analytical relations are analyzed which describe the trajectory and energy characteristics of guidance methods based on Legostaev and Raushenbach's (1969) docking technique. The conditions for determining the optimal parameters required for performing the desired maneuver are examined, along with the combined use of impulsive and continuous control to achieve quasi-optimal docking.

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