Minimax evaluation of the accuracy of spacecraft orbit determination taking into account unmodeled accelerations

Details Minimax evaluation of the accuracy of spacecraft orbit determination taking into account unmodeled accelerations Minimax evaluation of the accuracy of spacecraft orbit determination taking into account unmodeled accelerations

May 1979

adsabs.harvard.edu/cgi-bin/nph-data_query?bibcode=1979kosis..17..355a&link_type=abstract

Kosmicheskie Issledovaniia, vol. 17, May-June 1979, p. 355-363. In Russian.

Physics

Acceleration (Physics), Celestial Mechanics, Minimax Technique, Orbit Perturbation, Satellite Orbits, Trajectory Optimization, Algorithms, Error Analysis, Integral Equations, Theorem Proving

Scientific paper

The paper considers the optimal processing of measurement data for determining orbits of planetary spacecraft taking into account unknown perturbing forces that induce so-called 'unmodeled' accelerations. Such perturbing forces may lead to significant position errors in the course of the flight of an interplanetary spacecraft. A minimax approach is taken to the accuracy problem and the structure of an optimal filter is considered.

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