Investigation of the orbital gyrocompassing problem by methods of the theory of linear observation systems

Details Investigation of the orbital gyrocompassing problem by methods of the theory of linear observation systems Investigation of the orbital gyrocompassing problem by methods of the theory of linear observation systems

Jul 1989

adsabs.harvard.edu/cgi-bin/nph-data_query?bibcode=1989kosis..27..502e&link_type=abstract

Kosmicheskie Issledovaniia (ISSN 0023-4206), vol. 27, July-Aug. 1989, p. 502-508. In Russian.

Computer Science

Gyrocompasses, Linear Systems, Orbital Position Estimation, Spacecraft Control, Differential Equations, Gyroscopic Stability

Scientific paper

It is demonstrated that the orbital gyrocompassing problem can be solved by the use of various types of observing instruments. Existing types of orbital gyrocompasses are investigated on the basis of a general approach. The possibility of improving the precision of orbital gyrocompassing using various types of instrument sets for evaluating and compensating the effects of errors of local-vertical plotters and gyro drifts is substantiated in principle.

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