NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Collections About News Help Login

Press Enter or click the Search button to begin your search.

Back to Results
New one-step integration methods of high accuracyNew numerical methods for solution of restricted three-body problem periodic trajectories and factors affecting accuracy and computer time through use of new methods
Document ID
19660018018
Acquisition Source
Legacy CDMS
Document Type
Other
Authors
Fehlberg, E. (NASA Marshall Space Flight Center Huntsville, AL, United States)
Date Acquired
August 3, 2013
Publication Date
January 1, 1966
Subject Category
Space Sciences
Accession Number
66N27308
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
TRAJECTORY ANALYSIS
COMPUTER METHOD
DIFFERENTIAL EQUATION
NUMERICAL INTEGRATION
Document Inquiry

Available Downloads

There are no available downloads for this record.

Related Records

IDRelationTitle19660018016Collected WorksResearch Achievements Review Series no. 20 - Mathematics and computation researchN66-27306 15-30Collected Works19660018016Collected WorksResearch Achievements Review Series no. 20 - Mathematics and computation research
No Preview Available