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NASA NTRS · 19820025886

Constrained multibody system dynamics: An automated approach

Abstract

The governing equations for constrained multibody systems are formulated in a manner suitable for their automated, numerical development and solution. The closed loop problem of multibody chain systems is addressed. The governing equations are developed by modifying dynamical equations obtained from Lagrange's form of d'Alembert's principle. The modifications is based upon a solution of the constraint equations obtained through a zero eigenvalues theorem, is a contraction of the dynamical equations. For a system with n-generalized coordinates and m-constraint equations, the coefficients in the constraint equations may be viewed as constraint vectors in n-dimensional space. In this setting the system itself is free to move in the n-m directions which are orthogonal to the constraint vectors.

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BibTeXRIS

Kamman, J. W., Huston, R. L.. 1982-10-01. Constrained multibody system dynamics: An automated approach. https://ntrs.nasa.gov/citations/19820025886

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