On a method for the autonomous refinement of the motion parameters of a orbital spacecraft

Details On a method for the autonomous refinement of the motion parameters of a orbital spacecraft On a method for the autonomous refinement of the motion parameters of a orbital spacecraft

Sep 1983

adsabs.harvard.edu/cgi-bin/nph-data_query?bibcode=1983kosis..21..798o&link_type=abstract

Kosmicheskie Issledovaniia (ISSN 0023-4206), vol. 21, Sept.-Oct. 1983, p. 798-802. In Russian.

Other

Autonomy, Circular Orbits, Equations Of Motion, Orbital Mechanics, Spacecraft Motion, Spacecraft Orbits, Algorithms, Data Processing, Gravitational Fields, Least Squares Method, Planetary Gravitation, Statistical Analysis

Scientific paper

The conditional and normal equations are obtained using formulas describing spacecraft motion in almost-circular orbits. The statistical processing of the navigation data is carried out on the basis of the least squares method. An analytical study of optimal measurement schemes is performed, and a simple algorithm for the autonomous refinement of the motion parameters of a spacecraft in the gravitational field of the earth (or other planet) is developed.

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