An alternative algorithm for the spacecraft information system with magnetometer and solar sensor

Details An alternative algorithm for the spacecraft information system with magnetometer and solar sensor An alternative algorithm for the spacecraft information system with magnetometer and solar sensor

Aug 2009

adsabs.harvard.edu/cgi-bin/nph-data_query?bibcode=2009cosre..47..330t&link_type=abstract

Cosmic Research, Volume 47, Issue 4, pp.330-336

Physics

45.40.Cc

Scientific paper

The possibility of identification of motion parameters of a low-orbit
spacecraft using readings of a three-axis magnetometer and solar
position sensor, without integration of the Euler’s dynamic
equations or direct measurement of the object’s angular velocity,
is considered.

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