Multi-structural estimation of an integrated navigation system of a reusable spacecraft

Details Multi-structural estimation of an integrated navigation system of a reusable spacecraft Multi-structural estimation of an integrated navigation system of a reusable spacecraft

Jun 2008

adsabs.harvard.edu/cgi-bin/nph-data_query?bibcode=2008cosre..46..238p&link_type=abstract

Cosmic Research, Volume 46, Issue 3, pp.238-243

Physics

95.10.Eg

Scientific paper

An approach to the synthesis of an integrated navigation system is considered for a reusable space-craft that performs an arbitrary spatial maneuver under the conditions of internal and external disturbances. The offered approach provides for a noise-suppressing solution of the navigation problem, both in a regular mode of spacecraft motion, and during its descent along the unplanned trajectory.

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