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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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51#
發(fā)表于 2025-3-30 11:43:18 | 只看該作者
52#
發(fā)表于 2025-3-30 13:06:50 | 只看該作者
Coordinate Transformations,... and . 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 . in the constituent equations.
53#
發(fā)表于 2025-3-30 18:02:18 | 只看該作者
54#
發(fā)表于 2025-3-30 22:52:32 | 只看該作者
Mathematical modeling of spacecraft,lysts will differ in their preference for various ways of formulating equations, one man choosing Lagrange’s equations, a second preferring Hamilton’s principle, and a third relying upon a Newton-Euler formulation, these differences are much less fundamental than the initial choice of a mathematical model of the vehicle.
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