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The determination of orbits using Picard iterationThe 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.
Document ID
19760003080
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Mikkilineni, R. P. (Tennessee Univ. Space Inst. Tullahoma, TN, United States)
Feagin, T. (Tennessee Univ. Space Inst. Tullahoma, TN, United States)
Date Acquired
August 8, 2013
Publication Date
August 1, 1975
Publication Information
Publication: NASA. Goddard Space Flight Center Flight Mech.(Estimation Theory Symp.
Subject Category
Astrodynamics
Accession Number
76N10168
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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IDRelationTitle19760003079Collected WorksFlight Mechanics/Estimation Theory Symposium19760003079Collected WorksFlight Mechanics/Estimation Theory Symposium
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