Determination of satellite attitude using angular-velocity measurements

Details Determination of satellite attitude using angular-velocity measurements Determination of satellite attitude using angular-velocity measurements

May 1985

adsabs.harvard.edu/cgi-bin/nph-data_query?bibcode=1985kosis..23..331p&link_type=abstract

Kosmicheskie Issledovaniia (ISSN 0023-4206), vol. 23, May-June 1985, p. 331-334. In Russian.

Physics

1

Algorithms, Angular Velocity, Intercosmos Satellites, Satellite Attitude Control, Satellite Orientation, Velocity Measurement, Nonlinear Equations, Satellite Rotation, Spacecraft Motion

Scientific paper

A nonlinear algorithm is developed for determining satellite attitude on
the basis of angular-velocity-sensor indications with sufficiently weak
limits on the satellite-rotation characteristics. The method is
illustrated by results for the Intercosmos-17 satellite with a passive
three-axis stabilization system in the orbital coordinate system.

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