Observability in the problem of the correction of inertial navigation systems with the aid of additional information from an artificial earth satellite

Details Observability in the problem of the correction of inertial navigation systems with the aid of additional information from an artificial earth satellite Observability in the problem of the correction of inertial navigation systems with the aid of additional information from an artificial earth satellite

May 1984

adsabs.harvard.edu/cgi-bin/nph-data_query?bibcode=1984kosis..22..390k&link_type=abstract

Kosmicheskie Issledovaniia (ISSN 0023-4206), vol. 22, May-June 1984, p. 390-398. In Russian.

Physics

Artificial Satellites, Inertial Navigation, Navigation Aids, Navigation Satellites, Observability (Systems), Distance, Spacecraft Communication

Scientific paper

Results of an observability analysis are used to demonstrate the
possibility of using information about the distance between an object
and a navigation satellite to correct inertial navigation systems. It is
shown that the utilization of this additional information makes it
possible to determine all the basic navigation parameters.

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