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Numerical orbit integration efficiency of the Delaunay-Similar elementsOrbit equations with a set of conservative and a set of nonconservative perturbing potentials were considered. Scheifele's DS formulation of these equations has dependent variables similar to Delaunay's orbital elements with the true anomaly as the independent variable. Efficiency curves of computing cost v.s. accuracy were constructed for Adams integrators of order of 2 through 15 with several correcting algorithms and for a Runga-Kutta integrator. Considering stability regions, choices were made for the optimally efficient integration modes for the DS elements. Integrating in these modes reduces computing costs for a specified accuracy.
Document ID
19750002901
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Pierce, S.
(Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA, United States)
Date Acquired
September 3, 2013
Publication Date
October 15, 1974
Subject Category
Astrodynamics
Report/Patent Number
JPL-TM-33-710
NASA-CR-140768
Report Number: JPL-TM-33-710
Report Number: NASA-CR-140768
Accession Number
75N10973
Funding Number(s)
CONTRACT_GRANT: NAS7-100
CONTRACT_GRANT: NGR-05-071-005
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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