Spacecraft flight dynamics problems are examined and new algorithms for their solution are proposed. The problems of increasing the accuracy of spacecraft motion determination from measurement data are investigated. An algorithm for controlling the aerodynamic descent of a circular orbit is analyzed. New approaches to the solution of some optimization problems are presented. (Author)
Study of Spacecraft Flight Dynamics
1976
200 pages
Report
No indication
English
Study of spacecraft flight dynamics
TIBKAT | 1976
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