NASA NTRS · 19760003080
The determination of orbits using Picard iteration
Abstract
The determination of orbits by using Picard iteration is reported. This is a direct extension of the classical method of Picard that has been used in finding approximate solutions of nonlinear differential equations for a variety of problems. The application of the Picard method of successive approximations to the initial value and the two point boundary value problems is given.
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Mikkilineni, R. P., Feagin, T.. 1975-08-01. The determination of orbits using Picard iteration. https://ntrs.nasa.gov/citations/19760003080
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