Algorithm of navigation and control for entry into the Martian atmosphere

Details Algorithm of navigation and control for entry into the Martian atmosphere Algorithm of navigation and control for entry into the Martian atmosphere

Jul 1979

adsabs.harvard.edu/cgi-bin/nph-data_query?bibcode=1979kosis..17..529b&link_type=abstract

Kosmicheskie Issledovaniia, vol. 17, July-Aug. 1979, p. 529-539. In Russian.

Physics

Atmospheric Entry, Digital Navigation, Mars Atmosphere, Mars Landing, Reentry Guidance, Aircraft Guidance, Algorithms, Graphs (Charts)

Scientific paper

A modulating-function method is used to construct a multistep descent guidance algorithm for precision landing of a spacecraft on the Martian surface. The method involves calculation of the phase coordinates of the center of mass of the spacecraft on the basis of a fundamental system of variational navigation equations, describing the descent process. Numerical modeling indicates that the proposed method assures high accuracy of landing within a descent corridor of approximately 100 km.

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