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Justification of thrust vector deflection of twin-engine unmanned aerial vehicle power plants

    Mykola Kulyk Affiliation
    ; Volodymir Kharchenko Affiliation
    ; Mykhailo Matiychyk Affiliation

Abstract


A new pattern of twin-engine power plant installation in an unmanned aerial vehicle of the conventional aerodynamic scheme is presented. Reasons for moments of harmful pitching and diving are identified and a method of elimination is suggested.


Dvimotorio bepiločio orlaivio traukos vektorių valdymo pagrindimas


Santrauka. Pateikta nauja dviejų variklių patalpinimo schema bepiločiame orlaivyje, turinčiame normalią aerodinaminę schemą. Nustatytos pavojingų polinkio momentų priežastys bei pasiūlyti jų pašalinimo būdai.


Reikšminiai žodžiai: bepilotis orlaivis (BO)traukos vektoriaus deformacijapolinkio momentai.


First published online: 14 Apr 2011


Keyword : unmanned aerial vehicle (UAV), thrust vectors deflection, adverse and recovery moments

How to Cite
Kulyk, M., Kharchenko, V., & Matiychyk, M. (2011). Justification of thrust vector deflection of twin-engine unmanned aerial vehicle power plants. Aviation, 15(1), 25-29. https://doi.org/10.3846/16487788.2011.566319
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Apr 14, 2011
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