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Titlebook: Dynamics of Flexible Spacecraft; Department of Genera Peter W. Likins,Robert E. Roberson,Jens Wittenburg Book 1971 CISM Udine 1971 Dynamics

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Substructure equations of motion,. and ..(. = 1,...,n) which represent the appendage unknowns, the equations of motion of the appendage ultimately consist of the 6n scalar second order differential equations of motion for the n nodal bodies. The present section, however, has the intermediate objective of providing an expression for
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Equations of motion collections of substructures,ways. In Section 2.3 on substructure equations, it was assumed in order to focus that the substructure was a finite element system and the adjacent body was rigid, but this is a very special case. The procedure to be followed in developing equations for systems of substructures depends very much on
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