Zobrazeno 1 - 10
of 17
pro vyhledávání: '"fixed-wing UAV simulation"'
Publikováno v:
Drones, Vol 7, Iss 10, p 601 (2023)
With the advantages of long-range flight and high payload capacity, large fixed-wing UAVs are often used in anti-terrorism missions, disaster surveillance, and emergency supply delivery. In the existing research, there is little research on the 3D mo
Externí odkaz:
https://doaj.org/article/93ba9df685264d5289b1ddc8f8387d11
Autor:
Příleský, Libor
Nowadays number of UAVs is still increasing. If we want to design their autopilot system, we need a simulation model to test and tune our autopilot design. This thesis is about creating such model fo small fixed wing UAV. This thesis contain informat
Externí odkaz:
http://www.nusl.cz/ntk/nusl-231205
Publikováno v:
44th AIAA Aerospace Sciences Meeting and Exhibit.
** U.S. Army's System Simulation and Development Directorate (SSDD), Redstone Arsenal, Alabama, 35898 Abstract Several engineering techniques and tools were used to improve the fidelity of the Shadow TM 200 six degree-of-freedom simulation developed
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::eae07af791d070be0d30ceb7e4535019
https://doi.org/10.2514/6.2006-640
https://doi.org/10.2514/6.2006-640
Conference
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Akademický článek
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Publikováno v:
Journal of Intelligent & Fuzzy Systems. 2023, Vol. 44 Issue 1, p1153-1168. 16p.
Control Algorithms, Kalman Estimation and Near Actual Simulation for UAVs: State of Art Perspective.
Publikováno v:
Drones (2504-446X); Jun2023, Vol. 7 Issue 6, p339, 21p
Publikováno v:
International Journal of Robust & Nonlinear Control; 1/25/2023, Vol. 33 Issue 2, p1065-1097, 33p
Autor:
Samuel Teague, Javaan Chahl
Publikováno v:
Machine Learning with Applications, Vol 4, Iss , Pp 100027- (2021)
Many common navigation solutions fall short when an aircraft’s GPS signal is either jammed or spoofed. This is typically due to the iterative nature of the estimation process, which requires an acceptably accurate initial estimate, or due to the ac
Externí odkaz:
https://doaj.org/article/0c8cce07642e49b8a83a3bc5f855a648
Publikováno v:
Journal of Intelligent & Fuzzy Systems. 44:1153-1168
Flight performance of unmanned aerial vehicles (UAVs) strongly depends on implemented attitude tracking control. For designing better controllers, nonlinear control design techniques are often opted instead of control design based on linearized model
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::3519d4b82d6be59a71f7e6a425b1f90c
https://doi.org/10.3233/jifs-222630
https://doi.org/10.3233/jifs-222630