The Newton-Raphson method in orbit determination

Details The Newton-Raphson method in orbit determination The Newton-Raphson method in orbit determination

Dec 1986

adsabs.harvard.edu/cgi-bin/nph-data_query?bibcode=1986esasp.255..349g&link_type=abstract

In ESA Proceedings of the Second International Symposium on the Spacecraft Flight Dynamics p 349-354 (SEE N87-25354 19-18)

Statistics

Applications

Newton-Raphson Method, Orbit Calculation, Satellite Orbits, Convergence, Equations Of Motion, Two Body Problem

Scientific paper

Applications of the Newton-Raphson iterative method to artificial satellite orbit determination are reviewed. Solution of the nonlinear algebraic equation system is discussed and the convergence of the method is investigated. In the numerical examples, the equation which describes the motion of the satellite is the equation of the two-body motion. The state equation can involve any acting forces.

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