2001
DOI: 10.1006/jsvi.2001.3689
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Active Structural Control Based on the Prediction and Degree of Stability

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Cited by 32 publications
(17 citation statements)
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“…() developed an approximately optimal closed‐open‐loop control based on the prediction of near‐future excitations provided that a given norm criteria is satisfied. Aldemir and Bakioglu () analytically solved the modified linear quadratic regulator (MLQR) problem including a parameter representing system stability order in the presence of unknown seismic excitations. Mei et al.…”
Section: Introductionmentioning
confidence: 99%
“…() developed an approximately optimal closed‐open‐loop control based on the prediction of near‐future excitations provided that a given norm criteria is satisfied. Aldemir and Bakioglu () analytically solved the modified linear quadratic regulator (MLQR) problem including a parameter representing system stability order in the presence of unknown seismic excitations. Mei et al.…”
Section: Introductionmentioning
confidence: 99%
“…Owing to recent developments of digital control and measurement techniques, semiactive and active control techniques in the structural technology have received much attention (Bakioglu and Aldemir, 2001; Aldemir and Bakioglu, 2001; Aldemir, 2003, 2009; Saleh and Adeli, 1998b; Adeli and Saleh, 1998; Aldemir and Gavin, 2006; Alhan et al, 2006; Gavin and Aldemir, 2005). Active control methods are effective for a wide frequency range as well as for transient vibrations.…”
Section: Introductionmentioning
confidence: 99%
“…Because of the Heaviside step function in (2), analytical expressions for the frequency response function cannot be obtained. Frequency response functions for semiactively controlled structures can however be constructed by numerically integrating the system equations until a harmonic steady state is reached, and plotting the ratio of the response amplitude to the excitation amplitude as a function of the frequency ratio.…”
mentioning
confidence: 98%
“…The graphical representation of the continuous pseudo-skyhook control force (2) is also given in Fig. 1.…”
mentioning
confidence: 99%
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