Determination of the initial conditions of space vehicle entry into the Martian atmosphere, using a detachable navigation probe

Details Determination of the initial conditions of space vehicle entry into the Martian atmosphere, using a detachable navigation probe Determination of the initial conditions of space vehicle entry into the Martian atmosphere, using a detachable navigation probe

Jul 1980

adsabs.harvard.edu/cgi-bin/nph-data_query?bibcode=1980kosis..18..507i&link_type=abstract

Kosmicheskie Issledovaniia, vol. 18, July-Aug. 1980, p. 507-517. In Russian.

Mathematics

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

Scientific paper

The paper deals with the determination of the vector of state for a Martian entry in the case where navigational information is provided by a probe ejected from the vehicle. The physical conditions are examined. The problem of determining the state vector is formulated, and algorithms for solving the problem are proposed. The effectiveness of the algorithms in the presence of various disturbing factors is assessed on the basis of numerical results.

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