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Coordinate Transformations

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Dynamics of Flexible Spacecraft

Part of the book series: International Centre for Mechanical Sciences ((CISM,volume 103))

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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

$$q\mathop = \limits^\Delta {\left[ {u_1^1u_2^1u_3^1\beta _1^1\beta _2^1\beta _3^1u_2^1...\beta _3^n} \right]^T}$$
(63)

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

$$M'\ddot q + D'\dot q + G'\dot q + K'q + A'q = L'$$
(64)

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

  • eBook Packages: Springer Book Archive

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