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Published online by Cambridge University Press: 14 August 2015
The main points of the method of partial anomalies are described. The method makes it possible to obtain analytical solutions for comets moving in orbits with high eccentricities. The method may be applied, in particular, to systems in which the orbits of the disturbed and disturbing bodies have points equidistant from the Sun. The method is applied to the calculation of the general perturbations by Saturn on P/Tuttle.