Physics
Scientific paper
Jul 1980
adsabs.harvard.edu/cgi-bin/nph-data_query?bibcode=1980kosis..18..518a&link_type=abstract
Kosmicheskie Issledovaniia, vol. 18, July-Aug. 1980, p. 518-526. In Russian.
Physics
Dynamic Control, Equations Of Motion, Iterative Solution, Newton Methods, Newton Theory, Orbit Calculation, Spacecraft Orbits, Algorithms, Convergence, Differential Equations, Motion Stability, Nonlinear Equations, Statistical Analysis
Scientific paper
An iterative algorithm is proposed for solving the problem of statistical data-processing for differential determination of a spacecraft orbit. The algorithm permits development of a stable procedure for evaluating the parameters of spacecraft motion without the need of calculating higher-order derivatives. The method is based on the concept of Newton-Kantorovich-type regularized processes which, in combination with an effective method of determining the regularization parameter, yield the required effect.
Arutiunov S. K.
Brzhozovskii A. E.
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