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Eliminating Computational Instability In Multibody SimulationsTWOBODY implements improved version of Lagrange multiplier method. Program ultilizes programming technique eliminating computational instability in multibody simulations in which Lagrange multipliers used. In technique, one uses constraint equations, instead of integration, to determine coordinates that are not independent. To illustrate technique, it includes simple mathematical model of solid rocket booster and parachute connected by frictionless swivel. Written in FORTRAN 77.
Document ID
19940000513
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Tech Brief
Authors
Watts, Gaines L.
(NASA Marshall Space Flight Center, Huntsville, AL.)
Date Acquired
August 16, 2013
Publication Date
September 1, 1994
Publication Information
Publication: NASA Tech Briefs
Volume: 18
Issue: 9
ISSN: 0145-319X
Subject Category
Mechanics
Report/Patent Number
MFS-28774
Accession Number
94B10513
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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