Soft landing dynamics of spherical landing modules

Details Soft landing dynamics of spherical landing modules Soft landing dynamics of spherical landing modules

Jul 1990

adsabs.harvard.edu/cgi-bin/nph-data_query?bibcode=1990kosis..28..539p&link_type=abstract

Kosmicheskie Issledovaniia (ISSN 0023-4206), vol. 28, July-Aug. 1990, p. 539-544. In Russian.

Computer Science

Dynamic Tests, Planetary Surfaces, Soft Landing, Spacecraft Landing, Spheres, Venera 7 Satellite, Venera 8 Satellite

Scientific paper

A method is described for analyzing the soft landing dynamics of spherical landing modules in the case where the landing velocity has a component parallel to the landing surface. Changes in the motion parameters of a spacecraft with time and in relation to the surface inclination are examined as an example. The approach proposed here can be used for both spherical landing modules and modules whose front surface is part of a sphere.

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