Zobrazeno 1 - 5
of 5
pro vyhledávání: '"Franciszek Dul"'
Publikováno v:
Energies, Vol 13, Iss 20, p 5354 (2020)
This paper presents a controller design process for an aircraft tracking problem when not all states are available. In the study, a nonlinear-transport aircraft simulation model was used and identified through Maximum Likelihood Principle and Extende
Externí odkaz:
https://doaj.org/article/254e3d7e442a4e1d870dcbb24f7a1213
Publikováno v:
Sensors, Vol 20, Iss 10, p 2955 (2020)
In this paper, the full tracking problem in aircraft system identification and control is presented. Time domain output error method with maximum likelihood principle was used to perform system identification. The linear quadratic regulator (LQR)-bas
Externí odkaz:
https://doaj.org/article/f27b4b24bdd948a0bc1ee2fc13c8e4e0
Autor:
Franciszek Dul
Publikováno v:
Mechanika w Lotnictwie ML-XX 2022 ISBN: 9788361021667
Modelowanie obiektów latających jest niezbędne przy budowie symulatorów wszelkich rodzajów. Celem modelowania jest symulowanie ruchu obiektów w taki sposób, aby odwzorowane zachowania samolotu były akceptowalne przez pilotów. Modelowanie kla
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::79d94fc5d91ab845222a09f2ac91eaf9
https://doi.org/10.15632/ml2022/15-30
https://doi.org/10.15632/ml2022/15-30
Autor:
Franciszek Dul
Publikováno v:
Aircraft Engineering and Aerospace Technology. 91:420-427
PurposeThe purpose of the paper is to analyze the active suppression of the aeroelastic vibrations of ailerons with strongly nonlinear characteristics by neural network/reinforcement learning (NN/RL) control method and comparing it with the classic r
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::ee337109045709d8720c8fe7f0c1fac5
https://doi.org/10.1108/aeat-01-2018-0019
https://doi.org/10.1108/aeat-01-2018-0019
Autor:
Franciszek Dul
Publikováno v:
Aircraft Engineering and Aerospace Technology. 90:688-698
Purpose The purpose of this paper is to analyze the active suppression of the nonlinear aeroelastic vibrations of ailerons caused by freeplay by robust H∞ and linear quadratic Gauss (LQG) methods of control in case of incomplete measurements of the
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::55ea75daf8f06bb03b55f10491247b57
https://doi.org/10.1108/aeat-11-2016-0215
https://doi.org/10.1108/aeat-11-2016-0215