Commenced in January 2007
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Paper Count: 30296
Conceptual Design of Unmanned Aerial Targets

Authors: M. Adamski, J. Cwiklak

Abstract:

The contemporary battlefield creates a demand for more costly and highly advanced munitions. Training personnel responsible for operations as well as immediate execution of combat tasks which engage real asset is unrealistic and economically not feasible. Owing to a wide array of exploited simulators and various types of imitators, it is possible to reduce the costs. One of the effective elements of training, which can be applied in the training of all service branches, is imitator of aerial targets. This research serves as an introduction to the commencement of design analysis over a real aerial target imitator. Within the project, the basic aerodynamic calculations were made, which enabled to determine its geometry, design layout, performance as well as mass balance of individual components. The conducted calculations of the parameters of flight characteristics come closer to the real performance of such Unmanned Aerial Vehicles.

Keywords: Aerodynamics, Performance, aerial target, imitator

Digital Object Identifier (DOI): doi.org/10.5281/zenodo.1109970

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[1] Adamski M., Rajchel J., „Bezzałogowe Statki Powietrzne, cz. I, Charakterystyka i wykorzystanie”, WSOSP-Dęblin, 2013.
[2] Danielecki S., Projektowanie samolotów, Oficyna Wydawnicza Politechniki Warszawskiej, Warszawa, 2000.
[3] Fiszdon W., Mechanika lotu , PWN, Warszawa – Łódź, 1961.
[4] Grzesik N., Infrared passive homing guidance gun system on UCAV, Scientific Aspects of Unmanned Mobile Vehicle, Politechnika Świętokrzyska, Kielce, 2010.
[5] Grzegorzewski M., Ciećko A., Oszczak S., Ćwiklak J., Aircraft Landing System Utilizing a GPS Receiver with Position Prediction Capability/Functionality, ION GNSS 2011. Portland USA.
[6] Jankowska-Sieminska B., Jankowski A., Slezak M., Analysis and Research of Piston Working Conditions of Combustion Engine in High Thermal Load Conditions, Journal f KONES 2007, Vol. 14, No. 3.
[7] Jel R., Projekt wstępny imitatora celu powietrznego., Praca mgr WSOSP-Dęblin, 2010.
[8] Koruba Z., Dziopa Z., Krzysztofik I., Dynamics of a Controlled Antiaircraft Missile Launcher Mounted on a Moveable Base, Journal of Theoretical and Applied Mechanics, Vol. 48, No. 2, 2010.
[9] Pila J., Kozuba J., Korba P., Airframe Structure, Dęblin, 2014.
[10] Warchulski J., Czechowicz B., Opracowanie projektu systemu imitatorów celów powietrznych do strzelań rakietowych ICP-SR, Warszawa, 2007.
[11] Zyluk A., Numerical simulation of the Effect of Wind on the Missile Motion, Journal of Theoretical and Applied Mechanics, 52/2, 2014.