Optimal entry probe trajectories with two-dimensional control in the Martian atmosphere

Details Optimal entry probe trajectories with two-dimensional control in the Martian atmosphere Optimal entry probe trajectories with two-dimensional control in the Martian atmosphere

May 1977

adsabs.harvard.edu/cgi-bin/nph-data_query?bibcode=1977cosre..14..798s&link_type=associated

(Kosmicheskie Issledovaniia, vol. 14, Nov.-Dec. 1976, p. 936-943.) Cosmic Research, vol. 14, no. 6, May 1977, p. 798-804. Trans

Physics

Mars Atmosphere, Mars Landing, Spacecraft Control, Terminal Velocity, Trajectory Optimization, Angle Of Attack, Boundary Value Problems, Calculus Of Variations, Lift Drag Ratio, Maximum Principle, Optimal Control

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