The use of an optimal-correction algorithm for estimation with unsimulated accelerations

Details The use of an optimal-correction algorithm for estimation with unsimulated accelerations The use of an optimal-correction algorithm for estimation with unsimulated accelerations

May 1988

adsabs.harvard.edu/cgi-bin/nph-data_query?bibcode=1988kosis..26..339l&link_type=abstract

Kosmicheskie Issledovaniia (ISSN 0023-4206), vol. 26, May-June 1988, p. 339-352. In Russian.

Astronomy and Astrophysics

Astronomy

Astrodynamics, Minimax Technique, Satellite Orbits, Algorithms, Circular Orbits, Correction

Scientific paper

It is demonstrated that the minimax problem involving the estimation of motion parameters in the presence of unsimulated acceleration can be solved efficiently using an algorithm developed for solving the problem of generalized linear pulsed correction. Calculations are performed for different variants of the estimation of the plane-motion parameters of a satellite in nearly circular orbit for different relationships between the limiting values of the unsimulated acceleration and measurement errors. Their algorithm complexity is discussed along with the relationship between the exact solution and the solution of simplified variants of the problem.

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