The use of dynamics equations in the synthesis of algorithms of attitude determination

Details The use of dynamics equations in the synthesis of algorithms of attitude determination The use of dynamics equations in the synthesis of algorithms of attitude determination

Jan 1992

adsabs.harvard.edu/cgi-bin/nph-data_query?bibcode=1992kosis..30...38e&link_type=abstract

Kosmicheskie Issledovaniia (ISSN 0023-4206), vol. 30, no. 1, Jan.-Feb. 1992, p. 38-44. In Russian.

Mathematics

Equations Of Motion, Satellite Attitude Control, Satellite Orientation, Angular Velocity, Dynamic Characteristics, Matrices (Mathematics), State Vectors

Scientific paper

The paper examines the synthesis of algorithms for the processing of measurement data in spacecraft attitude determination systems using methods of observation system theory. It is noted that, in the case of such synthesis, it is useful to consider not only the kinematic but also the dynamic equations of the spacecraft's rotation. The use of such additional a priori information can make it possible to reduce the number of measuring instruments or to enhance the attitude accuracy with the same number of measuring instruments.

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