Determination of the initial conditions of entry of a spacecraft into the Martian atmosphere using a separable navigational probe

Details Determination of the initial conditions of entry of a spacecraft into the Martian atmosphere using a separable navigational probe Determination of the initial conditions of entry of a spacecraft into the Martian atmosphere using a separable navigational probe

Jan 1981

adsabs.harvard.edu/cgi-bin/nph-data_query?bibcode=1981cosre..18..362i&link_type=associated

(Kosmicheskie Issledovaniia, vol. 18, July-Aug. 1980, p. 507-517.) Cosmic Research, vol. 18, no. 4, Jan. 1981, p. 362-371. Tran

Mathematics

Atmospheric Entry, Dynamic Control, Mars Atmosphere, Space Navigation, Spacecraft Trajectories, Algorithms, Mathematical Models, Matrices (Mathematics), Trajectory Optimization

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