Aircraft longitudinal motion control based on Takagi-Sugeno fuzzy model

Result code in IS VaVaI
<a href="https://www.isvavai.cz/riv?ss=detail&h=RIV%2F68407700%3A21230%2F16%3A00307613" target="_blank" >RIV/68407700:21230/16:00307613 - isvavai.cz</a>
Result on the web
<a href="http://dx.doi.org/10.1016/j.asoc.2016.07.038" target="_blank" >http://dx.doi.org/10.1016/j.asoc.2016.07.038</a>
DOI - Digital Object Identifier
<a href="http://dx.doi.org/10.1016/j.asoc.2016.07.038" target="_blank" >10.1016/j.asoc.2016.07.038</a>

Result language
angličtina
Original language name
Aircraft longitudinal motion control based on Takagi-Sugeno fuzzy model
Original language description
Fuzzy logic control of longitudinal motion of an aircraft based on Takagi-Sugeno modelling approach is presented in this paper. Takagi-Sugeno model of the motion along the desired trajectory is used for state-space parallel decomposition controller (PDC) design. The proposed control scheme guarantees stability of closed loop and asymptotical step pitch angle reference signal tracking. Simulation results on twin-engine short-range transport aircraft LET L410 indicate that the proposed control law can represent a feasible aircraft motion control technique and especially in presence of model inaccuracies and disturbances it overcomes the most commonly used approaches.
Czech name
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Czech description
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Type
J<sub>x</sub> - Unclassified - Peer-reviewed scientific article (Jimp, Jsc and Jost)
CEP classification
BC - Theory and management systems
OECD FORD branch
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Project
<a href="/en/project/GA16-21961S" target="_blank" >GA16-21961S: Mechatronic structures with haevily distributed actuators and sensors</a><br>
Continuities
P - Projekt vyzkumu a vyvoje financovany z verejnych zdroju (s odkazem do CEP)

Publication year
2016
Confidentiality
S - Úplné a pravdivé údaje o projektu nepodléhají ochraně podle zvláštních právních předpisů

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