A method of inertial navigation system correction using relative measurements by navigation satellites.

Details A method of inertial navigation system correction using relative measurements by navigation satellites. A method of inertial navigation system correction using relative measurements by navigation satellites.

Jul 1992

adsabs.harvard.edu/cgi-bin/nph-data_query?bibcode=1992cosre..30...49i&link_type=abstract

Cosmic Res., Vol. 30, No. 1, p. 49 - 54

Computer Science

Scientific paper

A method is proposed of correcting a spacecraft inertial navigation system during descent from orbit using a navigation satellite. The navigation information includes the components of apparent spacecraft acceleration and parameters of motion of its center of mass, obtained using accelerometers and the satellite navigation system. This method can be used to determine the orientation of the sensitivity axes of the inertial navigation system. The dependence of the method's precision on statistical properties of perturbations is studied.

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