Vibration Control of Flexible Aircraft with Respect to Passengers Comfort
The result's identifiers
Result code in IS VaVaI
<a href="https://www.isvavai.cz/riv?ss=detail&h=RIV%2F68407700%3A21220%2F10%3A00178809" target="_blank" >RIV/68407700:21220/10:00178809 - isvavai.cz</a>
Result on the web
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DOI - Digital Object Identifier
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Alternative languages
Result language
angličtina
Original language name
Vibration Control of Flexible Aircraft with Respect to Passengers Comfort
Original language description
The paper deals with the development of the active vibration suppression of fuselage of flexible aircraft of BWB (blended wing body) type with respect to comfort criterions. The independent system of the proof mass actuators within the fuselage is considered as actuators, accelerometers throughout the fuselage are considered as the sensors. The placement of actuators and sensors is optimized through the special norms minimization. The feedback control design is done by H inf. method. The robustness of the controller is tested with respect to the fuel and passengers mass variations.
Czech name
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Czech description
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Classification
Type
D - Article in proceedings
CEP classification
BC - Theory and management systems
OECD FORD branch
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Result continuities
Project
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Continuities
R - Projekt Ramcoveho programu EK
Others
Publication year
2010
Confidentiality
S - Úplné a pravdivé údaje o projektu nepodléhají ochraně podle zvláštních právních předpisů
Data specific for result type
Article name in the collection
Proceedings of ISMA2010, International Conference on Noise and Vibration Engineering, including USD2010
ISBN
978-90-73802-87-2
ISSN
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e-ISSN
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Number of pages
13
Pages from-to
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Publisher name
Katholieke Universiteit
Place of publication
Leuven
Event location
Leuven
Event date
Sep 20, 2010
Type of event by nationality
WRD - Celosvětová akce
UT code for WoS article
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