Application of duality theory to the estimation of the accuracy of spacecraft orbital parameters

Details Application of duality theory to the estimation of the accuracy of spacecraft orbital parameters Application of duality theory to the estimation of the accuracy of spacecraft orbital parameters

Nov 1985

adsabs.harvard.edu/cgi-bin/nph-data_query?bibcode=1985kosis..23..849b&link_type=abstract

Kosmicheskie Issledovaniia (ISSN 0023-4206), vol. 23, Nov.-Dec. 1985, p. 849-862. In Russian.

Astronomy and Astrophysics

Astronomy

Astrodynamics, Duality Principle, Orbit Calculation, Satellite Orbits, Algorithms, Integral Equations, Iteration, Theorem Proving

Scientific paper

A relationship is established between the problem of the optimal selection of the set of measurements and a pair of dual problems obtained through the application of a specified theorem to the best-approximation problem. An algorithm for the optimal selection of the set of measurements under the effect of nonsimulated acceleration is presented. A linear programming approach is used throughout.

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