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Attitude dynamics simulation subroutines for systems of hinge-connected rigid bodies with nonrigid appendagesThree computer subroutines designed to solve the vector-dyadic differential equations of rotational motion for systems that may be idealized as a collection of hinge-connected rigid bodies assembled in a tree topology, with an optional flexible appendage attached to each body are reported. Deformations of the appendages are mathematically represented by modal coordinates and are assumed small. Within these constraints, the subroutines provide equation solutions for (1) the most general case of unrestricted hinge rotations, with appendage base bodies nominally rotating at a constant speed, (2) the case of unrestricted hinge rotations between rigid bodies, with the restriction that those rigid bodies carrying appendages are nominally nonspinning, and (3) the case of small hinge rotations and nominally nonrotating appendages. Sample problems and their solutions are presented to illustrate the utility of the computer programs.
Document ID
19760005003
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Fleischer, G. E.
(Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA, United States)
Likins, P. W.
(Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA, United States)
Date Acquired
September 3, 2013
Publication Date
August 15, 1975
Subject Category
Astrodynamics
Report/Patent Number
NASA-CR-145794
JPL-TR-32-1598
Accession Number
76N12091
Funding Number(s)
CONTRACT_GRANT: NAS7-100
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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