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Wyszukujesz frazę "unmanned aerial systems" wg kryterium: Temat


Wyświetlanie 1-5 z 5
Tytuł:
The Quality of Unmanned Aerial Vehicles: Ergodesign Aspect. Part 2
Autorzy:
Kharchenko, Volodymyr
Rubtsov, Anatolii
Svirko, Volodymyr
Zhudova, Iryna
Powiązania:
https://bibliotekanauki.pl/articles/2056522.pdf
Data publikacji:
2022-06-07
Wydawca:
Międzynarodowa Wyższa Szkoła Logistyki i Transportu
Tematy:
unmanned aerial vehicle
ergodesign aspect
aerial systems
Opis:
In the modern world, scientific and practical ergodesign activity on the development and use of drones, the concept of "human factor" is becoming more and more important. It is one of the main studies in improving the safety, efficiency and comfort of the "man - unmanned aerial vehicle" system operation. The most promising research is aimed at the application and development of new approaches to the evaluation of algorithms for unmanned aircraft maintenance and the organization of their operators` activities. The system of unmanned aerial vehicles ergodesign quality indicators developed and presented in a tabular form reflects practically all design and ergonomic properties of modern unmanned aerial systems. It is based on the existing normative documentation inUkrainedeveloped by the authors, harmonized with international and European standards. It allows the analysis and evaluation of unmanned aerial vehicles in order to take into account consumer interests at the beginning of their design reducing the assimilation time of products and preventing irrational production costs. The results of such an analysis underlie the development of technical documentation, standards, and specifications. They should be taken into account when putting products into production.
Źródło:
Logistics and Transport; 2022, 53-54, 1-2; 133-160
1734-2015
Pojawia się w:
Logistics and Transport
Dostawca treści:
Biblioteka Nauki
Artykuł
Tytuł:
Integration and in-field gains selection of flight and navigation controller for remotely piloted aircraft system
Autorzy:
Słowik, M.
Ołdziej, D.
Gosiewski, Z.
Powiązania:
https://bibliotekanauki.pl/articles/386917.pdf
Data publikacji:
2017
Wydawca:
Politechnika Białostocka. Oficyna Wydawnicza Politechniki Białostockiej
Tematy:
remotely piloted aircraft systems
unmanned aerial vehicle
autopilot
flight controller
navigation controller
Opis:
In the paper the implementation process of commercial flight and navigational controller in own aircraft is shown. The process of autopilot integration were performed for the fixed-wing type of unmanned aerial vehicle designed in high-wing and pull configuration of the drive. The above equipment were integrated and proper software control algorithms were chosen. The correctness of chosen hardware and software solution were verified in ground tests and experimental flights. The PID controllers for longitude and latitude controller channels were selected. The proper deflections of control surfaces and stabilization of roll, pitch and yaw angles were tested. In the next stage operation of telecommunication link and flight stabilization were verified. In the last part of investigations the preliminary control gains and configuration parameters for roll angle control loop were chosen. This enable better behavior of UAV during turns. Also it affected other modes of flight such as loiter (circle around designated point) and auto mode where the plane executed a pre-programmed mission.
Źródło:
Acta Mechanica et Automatica; 2017, 11, 1; 33-37
1898-4088
2300-5319
Pojawia się w:
Acta Mechanica et Automatica
Dostawca treści:
Biblioteka Nauki
Artykuł
Tytuł:
Computationaly simple obstacle avoidance control law for small unmanned aerial vehicles
Autorzy:
Cieśluk, J.
Gosiewski, Z.
Ambroziak, L.
Romaniuk, S.
Powiązania:
https://bibliotekanauki.pl/articles/386705.pdf
Data publikacji:
2015
Wydawca:
Politechnika Białostocka. Oficyna Wydawnicza Politechniki Białostockiej
Tematy:
unmanned aerial vehicle
quadrotor control
obstacle avoidance
vision systems
statki powietrzne bezzałogowe
unikanie przeszkód
Opis:
The investigations of the system which allow to avoid obstacles by the unmanned aerial vehicles (UAV) are presented in the paper. The system is designed to enable the full autonomous UAV flight in an unknown environment. As an information source about obstacles digital camera was used. Developed algorithm uses the existing relations between the imaging system and the parameters read from the UAV autopilot. Synthesis of the proposed obstacle avoidance control law was oriented for computational simplicity. Presented algorithm was checked during simulation studies and in-flight tests.
Źródło:
Acta Mechanica et Automatica; 2015, 9, 1; 50-56
1898-4088
2300-5319
Pojawia się w:
Acta Mechanica et Automatica
Dostawca treści:
Biblioteka Nauki
Artykuł
Tytuł:
Certification of Unmanned Aircraft (UA)
Autorzy:
Pettke, G.
Kozyro, W.
Gałka, P.
Trzeciak, G.
Wołejsza, P.
Powiązania:
https://bibliotekanauki.pl/articles/1841555.pdf
Data publikacji:
2021
Wydawca:
Uniwersytet Morski w Gdyni. Wydział Nawigacyjny
Tematy:
unmanned vehicles
Polish Register of Shipping
PRS
Unmanned Aircraft
unmanned aerial vehicle
remotely piloted aircraft systems
ground control station
object’s recognition and classification awareness
vertical take-off and landing
Opis:
PRS (Polish Register of Shipping) is an expert institution acting on the international market, that - by conducting business for the benefit of the community - through the formulation of the requirements, survey and issue of the appropriate documents, assists State Administrations, Underwriters and customers in ensuring the safety of people, floating objects, land undertakings, carried cargo and the natural environment. PRS is a body accredited for certification of management systems, as well as a notified body in the European Commission for conducting product conformity assessment procedures with EU directives and regulations, and certify of personnel and processes. Subject and scope of the Publication The Publication defines requirements and procedures of conformity assessment process of Unmanned Aircraft (UA) and the technical possibilities of their use in the maritime economy segment. Purpose of the publication: Defining technical and formal requirements for design, construction and operation of the Unmanned Aircraft (UA), Determining the scope and methodology of conformity assessment process of Unmanned Aircraft (UA), Determining the technical possibilities of using Unmanned Aircraft (UA) in the maritime economy segment. The publication includes the following issues: basic principles and design requirements as well as technical regulations that ensure the design of the Unmanned Aircraft (UA), as a safe product in operation; the scope and methodology of conformity assessment of Unmanned Aircraft (UA); principles and scope of technical supervision over the Unmanned Aircraft (UA), requirements set by PRS in using Unmanned Aircraft (UA) on sea-going ships. The conclusions of the paper: indication of the way to obtain BSP certification, the basis for launching the procedure for developing the NO defence standard for the certification of ships and naval auxiliary units for cooperation with Unmanned Aircraft (UA).
Źródło:
TransNav : International Journal on Marine Navigation and Safety of Sea Transportation; 2021, 15, 1; 143-155
2083-6473
2083-6481
Pojawia się w:
TransNav : International Journal on Marine Navigation and Safety of Sea Transportation
Dostawca treści:
Biblioteka Nauki
Artykuł
Tytuł:
Uszkodzenia w systemach sterowania i nawigacji bezzałogowych obiektów latających
Faults in control and navigation systems of unmanned aerial vehicles
Autorzy:
Dołęga, B.
Rzucidło, P.
Powiązania:
https://bibliotekanauki.pl/articles/152753.pdf
Data publikacji:
2011
Wydawca:
Stowarzyszenie Inżynierów i Techników Mechaników Polskich
Tematy:
systemy sterowania i nawigacji
bezzałogowy obiekt latający
modelowanie
zwielokrotnienia
aircraft control and navigation systems
unmanned aerial vehicle
modelling
redundancy
Opis:
Artykuł przedstawia ogólne uwagi związane z tworzeniem systemów sterowania i nawigacji tolerujących uszkodzenia pojawiające się w ich elementach składowych. Główną uwagę zwrócono na uszkodzenia w układach wejścia. Jako przykład omówiono odtwarzanie uszkodzonych sygnałów pomiarowych za pomocą estymat wyznaczanych na drodze analizy modelowania procesów fizycznych zachodzących w rozpatrywanym systemie. Metodę tą zastosowano również do zademonstrowania możliwości wyznaczania zwielokrotnień umożliwiających przeprowadzenie diagnozy systemu.
The paper presents basic remarks about construction of fault tolerant control and navigation systems for UAV. Reliability and safety requirements can be fulfill with usage of redundancies. Presentation of different kinds of avionic redundancies with comments about their usage during fault appearance is an important part of the paper. The main authors' attention is paid to faults in input devices. Their first goal of UAV measurement devices is generating the information of high quality, but the information must be dependable. On the basis of the authors' work experience, the application of signal estimation with remarks about their precision is introduced. After the general information about the troubleshooting in UAV measurement systems, the usage of a complementary filter for calculations of the roll angle is presented. Moreover, two methods of roll angle estimation are given with comments. The comparison of two methods of navigation parameter calculation as the diagnostic method application is also described. The considered applications have specific feature of UAV avionics systems in the presence of faults.
Źródło:
Pomiary Automatyka Kontrola; 2011, R. 57, nr 9, 9; 1020-1023
0032-4140
Pojawia się w:
Pomiary Automatyka Kontrola
Dostawca treści:
Biblioteka Nauki
Artykuł
    Wyświetlanie 1-5 z 5

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