Physics
Scientific paper
Sep 1974
adsabs.harvard.edu/cgi-bin/nph-data_query?bibcode=1974kosis..12..701g&link_type=abstract
Kosmicheskie Issledovaniia, vol. 12, Sept.-Oct. 1974, p. 701-706. In Russian.
Physics
Aerodynamic Brakes, Descent Trajectories, Mars Landing, Retrothrust, Thrust Programming, Trajectory Optimization, Atmospheric Entry, Equations Of Motion, Jet Control, Lift Drag Ratio, Mars Atmosphere, Sequential Control, Terminal Velocity
Scientific paper
Methods of determining the optimum sequences of powered and aerodynamic
(passive) descent trajectories are studied on the basis of a program for
obtaining minimum terminal velocities by controlling the L/D ratio, and
on the basis of two versions of retrojet control. The effectiveness of
the programs is demonstrated by numerical examples.
Golubtsov V. G.
Mitroshin É. I.
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