Development of autonomous unmanned aerial vehicle for thermal inspection of large engineering structures based on dilution control technology. (Q94418): Difference between revisions
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(Created claim: summary (P836): The project involves the development, execution and testing of a driverless drone to perform thermal imaging inspections. As part of the work on the prototype, a dedicated solubilised regulator FLC will be designed and implemented. Commissioning of Logic Controllers for the control of the flight and the stabilisation of the unmanned aerial vehicle (s). Unmanned aerial vehicles (UAVs), as they are non-stationary, non-linear control objects, are u...) |
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| Property / summary | |||
The project involves the development, execution and testing of a driverless drone to perform thermal imaging inspections. As part of the work on the prototype, a dedicated solubilised regulator FLC will be designed and implemented. Commissioning of Logic Controllers for the control of the flight and the stabilisation of the unmanned aerial vehicle (s). Unmanned aerial vehicles (UAVs), as they are non-stationary, non-linear control objects, are unable to stabilise themselves and require system correction systems, for example in the so-called ‘hinge’. The vehicle shall be designed in such a way as to permit work in extremely difficult conditions (e.g. strong wind shocks, turbulence around the buildings). The design of an assumed operating stabiliser for a hinged flight model will be innovation on a global scale. The adjusters shall be designed individually for those unmanned aircraft models followed by the ceiling and then placed on a specific unit. An unmanned inspection drone project on the current market offer will be characterised by innovative functionalities: 1) modern construction: the platform will be very light and robust through the use of state-of-the-art certified carbon pre-impregnation. (2) Performance in pilotage: this is reflected in the minimum number of operations to be carried out. (3) Deassembled propellers: with a 5-minute demontage, the device can be stored in the boot of the field car. 4) vertical take-off and landing: the platform shall have a vertical take-off and landing capability. 5) stability during the so-called hinge. (English) | |||
| Property / summary: The project involves the development, execution and testing of a driverless drone to perform thermal imaging inspections. As part of the work on the prototype, a dedicated solubilised regulator FLC will be designed and implemented. Commissioning of Logic Controllers for the control of the flight and the stabilisation of the unmanned aerial vehicle (s). Unmanned aerial vehicles (UAVs), as they are non-stationary, non-linear control objects, are unable to stabilise themselves and require system correction systems, for example in the so-called ‘hinge’. The vehicle shall be designed in such a way as to permit work in extremely difficult conditions (e.g. strong wind shocks, turbulence around the buildings). The design of an assumed operating stabiliser for a hinged flight model will be innovation on a global scale. The adjusters shall be designed individually for those unmanned aircraft models followed by the ceiling and then placed on a specific unit. An unmanned inspection drone project on the current market offer will be characterised by innovative functionalities: 1) modern construction: the platform will be very light and robust through the use of state-of-the-art certified carbon pre-impregnation. (2) Performance in pilotage: this is reflected in the minimum number of operations to be carried out. (3) Deassembled propellers: with a 5-minute demontage, the device can be stored in the boot of the field car. 4) vertical take-off and landing: the platform shall have a vertical take-off and landing capability. 5) stability during the so-called hinge. (English) / rank | |||
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Revision as of 07:18, 6 March 2020
Project in Poland financed by DG Regio
| Language | Label | Description | Also known as |
|---|---|---|---|
| English | Development of autonomous unmanned aerial vehicle for thermal inspection of large engineering structures based on dilution control technology. |
Project in Poland financed by DG Regio |
Statements
1,241,830.88 zloty
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1,994,571.28 zloty
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76.33 percent
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1 August 2017
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31 July 2019
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SKY TRONIC SPÓŁKA Z OGRANICZONĄ ODPOWIEDZIALNOŚCIĄ
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51°7'34.7"N, 16°58'41.5"E
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Przedmiotem projektu jest opracowanie, wykonanie i przetestowanie prototypu bezzałogowego drona do wykonywania inspekcji termowizyjnych obiektów inżynieryjnych. W ramach prac nad prototypem zostanie zaprojektowany i zaimplementowany dedykowany regulator rozmyty FLC (ang. Fuzzy Logic Controller) do sterowania lotem i stabilizacji bezzałogowego drona inspekcyjnego. Bezzałogowe statki powietrzne, jako że są niestacjonarnymi, nieliniowymi obiektami sterowania, nie potrafią się samodzielnie stabilizować i wymagają układów korygujących niestabilność np. w tzw. zawisie. Pojazd zostanie opracowany w taki sposób, by umożliwić pracę w ekstremalnie trudnych warunkach (np.silne podmuchy wiatru, turbulencje wokół budynków). Zaprojektowanie działającego w założony sposób stabilizatora lotu, który dobrze funkcjonował w zawisie, dla modelu wielowirnikowa będzie innowacją na skalę światową. Regulatory rozmyte projektuje się indywidualnie dla wskazanych modeli bezzałogowców, a następnie stroi się je do konkretnego egzemplarza. Opracowany w ramach projektu bezzałogowy dron inspekcyjny w odniesieniu do aktualnej oferty rynku będzie charakteryzował się innowacyjnymi funkcjonalnościami: 1)Nowoczesną konstrukcją: platforma będzie bardzo lekka i wytrzymała dzięki zastosowaniu najnowocześniejszych, certyfikowanych preimpregnatów węglowych. 2)Intuicyjnością w pilotażu: objawia się to minimalną liczbą czynności do wykonania. 3)Demontowanymi śmigłami: dzięki demontowanym w 5 minut śmigłom urządzenie można przechowywać w bagażniku samochodu terenowego. 4)Pionowym startem i lądowaniem: platforma będzie posiadać zdolność pionowego startu i lądowania. 5)Stabilnością podczas tzw. zawisu. (Polish)
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The project involves the development, execution and testing of a driverless drone to perform thermal imaging inspections. As part of the work on the prototype, a dedicated solubilised regulator FLC will be designed and implemented. Commissioning of Logic Controllers for the control of the flight and the stabilisation of the unmanned aerial vehicle (s). Unmanned aerial vehicles (UAVs), as they are non-stationary, non-linear control objects, are unable to stabilise themselves and require system correction systems, for example in the so-called ‘hinge’. The vehicle shall be designed in such a way as to permit work in extremely difficult conditions (e.g. strong wind shocks, turbulence around the buildings). The design of an assumed operating stabiliser for a hinged flight model will be innovation on a global scale. The adjusters shall be designed individually for those unmanned aircraft models followed by the ceiling and then placed on a specific unit. An unmanned inspection drone project on the current market offer will be characterised by innovative functionalities: 1) modern construction: the platform will be very light and robust through the use of state-of-the-art certified carbon pre-impregnation. (2) Performance in pilotage: this is reflected in the minimum number of operations to be carried out. (3) Deassembled propellers: with a 5-minute demontage, the device can be stored in the boot of the field car. 4) vertical take-off and landing: the platform shall have a vertical take-off and landing capability. 5) stability during the so-called hinge. (English)
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Identifiers
RPDS.01.02.01-02-0033/17
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