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The N-BOD2 user's and programmer's manualA general purpose digital computer program was developed and designed to aid in the analysis of spacecraft attitude dynamics. The program provides the analyst with the capability of automatically deriving and numerically solving the equations of motion of any system that can be modeled as a topological tree of coupled rigid bodies, flexible bodies, point masses, and symmetrical momentum wheels. Two modes of output are available. The composite system equations of motion may be outputted on a line printer in a symbolic form that may be easily translated into common vector-dyadic notation, or the composite system equations of motion may be solved numerically and any desirable set of system state variables outputted as a function of time.
Document ID
19780013257
Acquisition Source
Legacy CDMS
Document Type
Technical Publication (TP)
Authors
Frisch, H. P.
(NASA Goddard Space Flight Center Greenbelt, MD, United States)
Date Acquired
September 3, 2013
Publication Date
February 1, 1978
Subject Category
Spacecraft Design, Testing And Performance
Report/Patent Number
NASA-TP-1145
G-7702-F22
Report Number: NASA-TP-1145
Report Number: G-7702-F22
Accession Number
78N21200
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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