53rd AIAA Aerospace Sciences Meeting 2015
DOI: 10.2514/6.2015-0260
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Reduced-Order Modeling of Continuous-Time State-Space Unsteady Aerodynamics

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Cited by 5 publications
(2 citation statements)
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“…Gillebaart and de Breuker [28] has tabulated and reviewed the four most popular model order reduction to solve unsteady aerodynamics state-space. In another paper by Besselink et al [29], few other methods are presented and reviewed for its application in structural dynamics, numerical computation, and in control.…”
Section: Aeroelastic Wing Model Reduction For Limited Frequency Bandmentioning
confidence: 99%
See 1 more Smart Citation
“…Gillebaart and de Breuker [28] has tabulated and reviewed the four most popular model order reduction to solve unsteady aerodynamics state-space. In another paper by Besselink et al [29], few other methods are presented and reviewed for its application in structural dynamics, numerical computation, and in control.…”
Section: Aeroelastic Wing Model Reduction For Limited Frequency Bandmentioning
confidence: 99%
“…The two papers provide the methods of model order reduction, these are: bounds the balanced realization error of BPOD, needs to be fine-tuned. The error margin tuning makes the method less robust, while POD does not guarantee the stability of its true state-space [28]. The BT method is very robust in characteristics as the method requires no input other than the required order of the ROM; this makes the method one of the most widely used model reduction methods.…”
Section: Aeroelastic Wing Model Reduction For Limited Frequency Bandmentioning
confidence: 99%