2001
DOI: 10.1006/jsvi.2001.3838
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A Non-Linear Inverse Vibration Problem of Estimating the External Forces for a System With Displacement-Dependent Parameters

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Cited by 33 publications
(16 citation statements)
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References 11 publications
(14 reference statements)
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“…However, this is normally not a source of concern, unless the state and costate problems for some reason are considered separately and discretized independently, see, for example [10]. The important issue is that the choice of spaces for x h , x h , k h and k h for the costate equation must be identical to the choice of spaces for the state equation.…”
Section: Discretized Newton Updatementioning
confidence: 98%
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“…However, this is normally not a source of concern, unless the state and costate problems for some reason are considered separately and discretized independently, see, for example [10]. The important issue is that the choice of spaces for x h , x h , k h and k h for the costate equation must be identical to the choice of spaces for the state equation.…”
Section: Discretized Newton Updatementioning
confidence: 98%
“…Equation (5). With the temporal discretization in mind, the costate and state equations are kept on weak form (in contrast to [10] where the costate and state equations are treated on strong form using Runge-Kutta methods for integration).…”
Section: Z(t)mentioning
confidence: 99%
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“…An inverse vibrations problem to monitor and inspect the structural integrity of multi-story building is formulated in [28], whereas an experimental approach based on vibration measurements is presented in [29] for crack identification in structural members. A crack detection technique based on a dynamic stiffness inverse vibration formulation is presented in [30,31]; within the same framework, a nonlinear inverse problem approach to estimate the external forces in displacement-dependent parameters models is presented in [32,33].…”
Section: Introductionmentioning
confidence: 99%
“…The conjugate gradient method is used to determine the unknown loading of a nonlinear single-degree-of-freedom system in [7,8]. An artificial neural network is used in [9] to find loads acting on aircraft wings.…”
Section: Introductionmentioning
confidence: 99%