Determination of a spacecraft orbit by means of Green's functions

Details Determination of a spacecraft orbit by means of Green's functions Determination of a spacecraft orbit by means of Green's functions

Jan 1979

adsabs.harvard.edu/cgi-bin/nph-data_query?bibcode=1979kosis..17....3r&link_type=abstract

Kosmicheskie Issledovaniia, vol. 17, Jan.-Feb. 1979, p. 3-9. In Russian.

Statistics

Computation

Celestial Mechanics, Green'S Functions, Orbit Calculation, Satellite Orbits, Boundary Value Problems, Differential Equations, Integral Equations, Nonlinear Equations

Scientific paper

Some aspects of improving the accuracy of orbital determination in the presence of scant data are examined, along with means of reducing the computational method. It is shown that the nonlinear boundary value problem to which such determinations may be reduced can be solved by means of Green's functions, both with the high precision desired and moderate computational labor.

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