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1
Content available Certification of Unmanned Aircraft (UA)
EN
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).
2
EN
In the paper implementation of a ground control station for UAV flight simulator is shown. The ground control station software is in cooperation with flight simulator, displaying various aircraft flight parameters. The software is programmed in C++ language and utilizes the windows forms for implementing graphical content. One of the main aims of the design of the application was to simplify the interface, simultaneously maintaining the functionality and the eligibility. A mission can be planned and monitored using the implemented map control supported by waypoint list.
PL
W artykule przedstawiono przenośny system umożliwiający planowanie i monitorowanie misji bezzałogowego aparatu latającego klasy mikro lub mini. System składa się z przenośnego mikrokomputera o wysokiej odporności środowiskowej, manipulatorów, dedykowanego oprogramowania opracowanego przez autorów referatu, pozycjonera anteny kierunkowej (lub rejestratora wideo), układów telemetrii, stacji meteorologicznej oraz układów zasilających. Opis systemu uzupełniono prezentacją procesów projektowania, realizacji oraz testów zintegrowanego układu interfejsów operatora. Testy wykonywano w warunkach laboratoryjnych (symulacje systemu BSP1 w trybie hardware in the loop), jak również w warunkach polowych. Próby terenowe prowadzano również w niekorzystnych warunkach pogodowych, chrakteryzujących się m.in.: temperaturą otoczenia -5°C, porywami wiatru dochodzącymi do ok. 60 km/h oraz słabymi opadami śniegu. Stację kontroli lotu testowano w lotach wykonywanych w trybie manualnym (sterowanie poprzez aparaturę RC2 , jak też manipulator NSKL3 ), w trybie stabilizacji wybranych parametrów lotu, jak też podczas lotów autonomicznych. Prowadzone testy dokumentowano w postaci fotograficznej, filmowej oraz poprzez rejestrację parametrów pracy systemu BSP (rejestrator pokładowy oraz rejestrator NSKL).
EN
The work presents the portable system of both micro and mini class capable of planning and monitoring unmanned aerial vehicle (UAV) mission. The system consists of a portable microcomputer characterized by high environmental resistance, keypads, dedicated software developed by the authors of the paper, a directional antenna positioner (or video recorder), telemetry systems, meteorological stations as well as power systems. The system description was supplemented by the presentation of processes of design, implementation and testing of the integrated system of operator’s interfaces. The tests were carried out in laboratory environment (simulations of the UAV system in the loop hardware mode), as well as in the field conditions. The field tests were carried out in adverse weather, with the ambient temperature of -5˚C, wind gusts of up to approximately 60 km/h and a weak snowfall. The flight control station was tested during flights performed in manual mode (with control via radio and Ground Flight Control Station manipulator), in the mode with selected flights parameters stabilised as well as in autonomous flights. The conducted tests were documented in the form of photographs, film as well as record of parameters of UAV system performance (through flight data recorder and Ground Flight Control Station recorder).
PL
W artykule przedstawiono wymagania stawiane Naziemnym Stacjom Kontroli Lotów do Bezzałogowych Aparatów Latających, a także ich wyposażenie. Dodatkowo poddano szczegółowej analizie ich działanie w czasie projektowania i wykonywania misji przez bezpilotowiec, a także podano kilka przykładów stacji wykorzystywanych przez Siły Zbrojne różnych państw.
EN
In the article there have been presented the requirements set on ground flight control stations for unmanned aerial vehicles as well as their equipment. Additionally, their performance was thoroughly analyzed during the design phase as well as during the implementation phase. Moreover, some examples of ground control stations used by Armed Forces of different countries have been given.
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