Zobrazeno 1 - 10
of 81
pro vyhledávání: '"Piotr Lichota"'
Publikováno v:
Studia Medyczne, Vol 37, Iss 4, Pp 349-353 (2021)
Reports on patients hospitalised due to inflammatory diseases of the soft tissues in the head suggest worsening of the course of the underlying disease in the case of coexisting infection with the SARS-CoV-2 virus. The cases of 2 patients with neck p
Externí odkaz:
https://doaj.org/article/45acf6e3920f45a28a28ae8e249f0f17
Publikováno v:
Studia Medyczne, Vol 37, Iss 2, Pp 140-144 (2021)
The purpose of this paper was to present a review of the scientific literature on carrying out typical otolaryngological procedures during the COVID-19 pandemic and periods of increased numbers of SARS-CoV-2 infections. The recommendations on reducin
Externí odkaz:
https://doaj.org/article/c3b714d9de074fd1b0c878d8bf4b068e
Autor:
Adrian Pawełek, Piotr Lichota
Publikováno v:
Bulletin of the Polish Academy of Sciences: Technical Sciences, Vol 70, Iss 2 (2022)
Quick development of computer techniques and increasing computational power allow for building high-fidelity models of various complex objects and processes using historical data. One of the processes of this kind is an air traffic, and there is a gr
Externí odkaz:
https://doaj.org/article/4750e48ebe044b29869e61745b28d184
Publikováno v:
Energies, Vol 16, Iss 5, p 2501 (2023)
Thrust vector control (TVC) might be used to control aircraft at large altitudes and in post-stall conditions when aerodynamic control surfaces are ineffective. This study demonstrated that the implementation of the TVC on high-speed aircraft is a re
Externí odkaz:
https://doaj.org/article/5210b213bafd4a8b84454b6964bb96ab
Publikováno v:
Sensors, Vol 22, Iss 11, p 4090 (2022)
Identification of a spinning projectile controlled with gasodynamic engines is shown in this paper. A missile model with a measurement inertial unit was developed from Newton’s law of motion and its aerodynamic coefficients were identified. This wa
Externí odkaz:
https://doaj.org/article/102e01c8d6a242be90d5f5a438eb9805
Publikováno v:
Sensors, Vol 22, Iss 9, p 3257 (2022)
The article presents the analysis of the impact point dispersion reduction using lateral correction thrusters. Two types of control algorithms are used and four sources of uncertainties are taken into account: aerodynamic parameters, thrust curve, in
Externí odkaz:
https://doaj.org/article/c9ae97e259114c86a5eeea424b8a2daf
Autor:
Piotr Lichota
Publikováno v:
Journal of Guidance, Control, and Dynamics. 46:350-361
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::5bf93c150efaef573a677b0303f14203
https://doi.org/10.2514/1.g006654
https://doi.org/10.2514/1.g006654
Autor:
Piotr Lichota
Publikováno v:
Colloquia Theologica Ottoniana, Vol 1 (2019)
With the end of World War II, the new division of borders destroyed the previous order throughout the country. To the areas inhabited by the Germans until the end of the war, also people from the so-called Central Poland began to arrive. They came he
Externí odkaz:
https://doaj.org/article/0a75522f260f4577b60d74ede5aad209
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
Autor:
Piotr Lichota
Publikováno v:
Aerospace, Vol 7, Iss 8, p 113 (2020)
Designing a reconfiguration system for an aircraft requires a good mathematical model of the object. An accurate model describing the aircraft dynamics can be obtained from system identification. In this case, special maneuvers for parameter estimati
Externí odkaz:
https://doaj.org/article/d1c96d7350a14db080e47d6593a14dda