Flight Tests of the Unmanned Helicopter ILX-27 – Some Selected Issues / Zagadnienia Prób W Locie Bezzałogowego Śmigłowca ILX-27
| Autor: | Jarosław Hajduk, Ryszard Sabak |
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| Rok vydání: | 2013 |
| Předmět: | |
| Zdroj: | Journal of KONBiN. 25:45-58 |
| ISSN: | 2083-4608 1895-8281 |
| DOI: | 10.2478/jok-2013-0067 |
| Popis: | The unmanned helicopter ILX-27 has been designed and developed under the NCBR (in English, NCRD - National Center for Research and Development) project on the “Unmanned helicopter - a special-purpose aerobot” carried out by the Institute of Aviation (IL) and the Air Force Institute of Technology (ITWL), both in Warsaw, and the Military Aviation Works No. 1 J.S.C. in Łódź (WZL Łódź). The helicopter in question is a design initiated and developed solely as an unmanned vehicle in the weight category (MTOW) of 1100 kg. It is the outcome of a complex approach to issues of the helicopter’s structure and aerodynamics, and those of controlling it at different flight phases. From the very beginning, flight tests of this unmanned helicopter have been carried out under the remote-control mode of operation. The paper has been intended to present the outcomes of some selected stages of the project, i.e. the study and tests of groundcontrol components, and the flight tests. |
| Databáze: | OpenAIRE |
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