Abstract
Free-free systems can move as a rigid body through space, the structure is so-called unconstrained. The stiffness matrix [K] is singular and therefore the flexibility matrix [G] = [K] -1 does not exist. Launch vehicles, aircraft and spacecraft are examples of free-free moving dynamic systems. In this chapter, a method, the inertia relief, will be derived to analyse free-free systems. The motion as a rigid body will be eliminated and a new set of applied loads (relative forces) will be used to analyse the elastic behaviour of the free-free system. In the following sections the relative motion, relative forces will be introduced and a definition of the inertia-relief flexibility matrix [G f] will be given.
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© 2004 Springer-Verlag Berlin Heidelberg
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Wijker, J. (2004). Free-free Dynamic Systems, Inertia Relief. In: Mechanical Vibrations in Spacecraft Design. Springer, Berlin, Heidelberg. https://doi.org/10.1007/978-3-662-08587-5_14
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DOI: https://doi.org/10.1007/978-3-662-08587-5_14
Publisher Name: Springer, Berlin, Heidelberg
Print ISBN: 978-3-642-07354-0
Online ISBN: 978-3-662-08587-5
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