Abstract
There remains the critical task of packaging Eqs. (53) and (62), with substitutions from Eq. (46), in a form convenient for the generation of coordinate transformations. To this end, let
be the (6n × 1) matrix of nodal deformation coordinates, and rewrite the 6n second order differential equations implied by Eqs. (46), (53), and (62) in the form
where M′, D′ and K′ are (6n × 6n) symmetric matrices and where G′ and A′ are (6n × 6n) skew-symmetric matrices, with L′ a (6n × 1) matrix not involving the deformation variables in q. Since Eqs. (53), (62), and (46) are all linear in the variables uj ,β j. and \({\bar y^j}\) contained within q, and since any square matrix can be written as the sum of symmetric and skew-symmetric parts, the possibility of expression of these equations in the form of Eq. (64) is guaranteed by the symmetric character of the coefficients of \({\ddot u^j},{\ddot \beta ^j}\,and\,{\ddot \bar y^j}\) in the constituent equations.
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© 1971 Springer-Verlag Wien
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Likins, P.W., Roberson, R.E., Wittenburg, J. (1971). Coordinate Transformations. In: Dynamics of Flexible Spacecraft. International Centre for Mechanical Sciences, vol 103. Springer, Vienna. https://doi.org/10.1007/978-3-7091-2908-1_5
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DOI: https://doi.org/10.1007/978-3-7091-2908-1_5
Publisher Name: Springer, Vienna
Print ISBN: 978-3-211-81199-3
Online ISBN: 978-3-7091-2908-1
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