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Optimizing simulated trajectoriesGeneral-purpose rigid-body six-degrees-of-freedom program is used to solve wide variety of atmospheric flight mechanics and orbital transfer problems. Written for analysis of powered or unpowered vehicles operation near rotating oblate planet, typical applications include: guidance and flight-control system simulation and analysis, loads and dispersion-type analysis.
Document ID
19770000420
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Tech Brief
Authors
Brauer, G. L. (Martin Marietta Corp.)
Habeger, A. R. (Martin Marietta Corp.)
Stevenson, R. (Martin Marietta Corp.)
Date Acquired
August 8, 2013
Publication Date
March 1, 1978
Publication Information
Publication: NASA Tech Briefs
Volume: 2
Issue: 4
ISSN: 0145-319X
Subject Category
Mechanics
Report/Patent Number
LAR-12089
ISSN: 0145-319X
Report Number: LAR-12089
Accession Number
77B10420
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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