Flexible aircraft lateral control law of low order

Result code in IS VaVaI

<a href="https://www.isvavai.cz/riv?ss=detail&h=RIV%2F68407700%3A21230%2F12%3A00187571" target="_blank" >RIV/68407700:21230/12:00187571 - isvavai.cz</a>

Result on the web

—

DOI - Digital Object Identifier

—

Result language

angličtina

Original language name

Flexible aircraft lateral control law of low order

Original language description

Overview of European collaborative project is presented in this paper and some results on lateral control law design for Blended Wing Body (BWB) type aircraft are given. Rigid body motions as well as flexible dynamic of the aircraft are considered. Recently developed Hinfinity optimization tools for fixed order robust controller are used to device lateral control augmentation system (CAS) with extremely low complexity.

Czech name

—

Czech description

—

Type

J_x - Unclassified - Peer-reviewed scientific article (Jimp, Jsc and Jost)

CEP classification

JU - Aeronautics, aerodynamics, aeroplanes

OECD FORD branch

—

Project

Result was created during the realization of more than one project. More information in the Projects tab.

Continuities

P - Projekt vyzkumu a vyvoje financovany z verejnych zdroju (s odkazem do CEP)

Publication year

2012

Confidentiality

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

Name of the periodical

Czech Aerospace

ISSN

1211-877X

e-ISSN

—

Volume of the periodical

2011

Issue of the periodical within the volume

2

Country of publishing house

CZ - CZECH REPUBLIC

Number of pages

4

Pages from-to

1-4

UT code for WoS article

—

EID of the result in the Scopus database

—