Optimization of linear filtering in a problem of spacecraft tracking

Details Optimization of linear filtering in a problem of spacecraft tracking Optimization of linear filtering in a problem of spacecraft tracking

Jul 1987

adsabs.harvard.edu/cgi-bin/nph-data_query?bibcode=1987kosis..25..545s&link_type=abstract

Kosmicheskie Issledovaniia (ISSN 0023-4206), vol. 25, July-Aug. 1987, p. 545-555. In Russian.

Physics

Equations Of Motion, Linear Filters, Optimization, Spacecraft Tracking, Algorithms, Error Analysis, Statistical Analysis

Scientific paper

The estimation of spacecraft motion parameters using linear-filtering algorithms is considered. Formulas are obtained for the calculation of estimation errors due to inaccurate information about acceleration and the third time-coordinate derivative. These formulas are used for the optimal selection of the time interval between measurements of filter parameters to obtain estimates with the required accuracy.

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