Problem of the optimum space turn of a spacecraft relative to the center of mass

Details Problem of the optimum space turn of a spacecraft relative to the center of mass Problem of the optimum space turn of a spacecraft relative to the center of mass

Jul 1975

adsabs.harvard.edu/cgi-bin/nph-data_query?bibcode=1975kosis..13..473s&link_type=abstract

Kosmicheskie Issledovaniia, vol. 13, July-Aug. 1975, p. 473-480. In Russian.

Physics

2

Center Of Gravity, Spacecraft Maneuvers, Three Dimensional Motion, Time Optimal Control, Algorithms, Angular Velocity, Euler Equations Of Motion, Fuel Consumption, Time Response, Trajectory Optimization, Turning Flight

Scientific paper

The problem is considered of the space turn of a spacecraft which
consists of two consecutive turns about the center of mass that are
optimum in their response time. Formulas are obtained for determining
the parameters of the consecutive turns and for estimating the response
time and fuel consumption of the active body.

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