Signal Shaper for Flexible Aircraft

Result code in IS VaVaI

<a href="https://www.isvavai.cz/riv?ss=detail&h=RIV%2F68407700%3A21230%2F16%3A00304490" target="_blank" >RIV/68407700:21230/16:00304490 - isvavai.cz</a>

Result on the web

<a href="http://radio.feld.cvut.cz/conf/poster/" target="_blank" >http://radio.feld.cvut.cz/conf/poster/</a>

DOI - Digital Object Identifier

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Result language

angličtina

Original language name

Signal Shaper for Flexible Aircraft

Original language description

Lightweight flexible blended-wing-body (BWB) aircraft concept seems as a highly promising configuration for future high capacity airliners which suffers from reduced stiffness. For a reference tracking controller often the flexible modes are excited causing unwanted oscillations. Thus, this paper focuses on designing a signal shaper for the flexible BW aircraft which track the reference while can cancelling the oscillatory effect of the aircraft. The signal shaping controller is developed based on the distributed zero vibration (DZV) principles. The simulation results show that using the DZV controller the wing root forces and moments are reduced. This reduction in the wing root moment's peaks provides potential structural benefits and weight savings.

Czech name

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Czech description

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Type

D - Article in proceedings

CEP classification

JU - Aeronautics, aerodynamics, aeroplanes

OECD FORD branch

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Project

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Continuities

S - Specificky vyzkum na vysokych skolach

Publication year

2016

Confidentiality

S - Úplné a pravdivé údaje o projektu nepodléhají ochraně podle zvláštních právních předpisů

Article name in the collection

Proceedings of the 20th International Scientific Student Conferenece POSTER 2016

ISBN

978-80-01-05950-0

ISSN

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e-ISSN

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Number of pages

4

Pages from-to

1-4

Publisher name

Czech Technical University in Prague

Place of publication

Praha

Event location

Praha

Event date

May 24, 2016

Type of event by nationality

WRD - Celosvětová akce

UT code for WoS article

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