Information Support for a Low-Orbit Spacecraft Using Magnetometer and Solar Sensor Readings

Details Information Support for a Low-Orbit Spacecraft Using Magnetometer and Solar Sensor Readings Information Support for a Low-Orbit Spacecraft Using Magnetometer and Solar Sensor Readings

Sep 2003

adsabs.harvard.edu/cgi-bin/nph-data_query?bibcode=2003cosre..41..485t&link_type=abstract

Cosmic Research, v. 41, Issue 5, p. 485-493 (2003).

Physics

Scientific paper

The problem of estimation of the orbital and attitude motion parameters
of a spacecraft using readings of a three-axis onboard magnetometer and
solar sensor with considerable uncertainty of the initial conditions is
solved. Primary attention is paid to improvement of the observability of
the desired parameters and acceleration of the estimation process.

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