Abstract
In the systems analysed so far, the mass was assumed to be rigidly attached to the actuator. Although this is a valid assumption for the majority of industrial applications, there are some cases in which an allowance for the elasticity of either the mass itself or the member attaching it to the actuator has to be made. Aircraft powered flying controls are a typical example of an elastic mass system.
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© 2000 Springer Science+Business Media Dordrecht
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Walters, R.B. (2000). Elastically Mounted Mass Systems. In: Hydraulic and Electric-Hydraulic Control Systems. Springer, Dordrecht. https://doi.org/10.1007/978-94-015-9427-1_24
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DOI: https://doi.org/10.1007/978-94-015-9427-1_24
Publisher Name: Springer, Dordrecht
Print ISBN: 978-94-015-9429-5
Online ISBN: 978-94-015-9427-1
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