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Justification of thrust vector deflection of twin-engine unmanned aerial vehicle power plants / Dvimotorio bepiločio orlaivio traukos vektorių valdymo pagrindimas

    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.


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


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

How to Cite
[1]
Kulyk, M., Kharchenko, V. and Matiychyk, M. 2011. Justification of thrust vector deflection of twin-engine unmanned aerial vehicle power plants / Dvimotorio bepiločio orlaivio traukos vektorių valdymo pagrindimas. Aviation. 15, 1 (Apr. 2011), 25-29. DOI:https://doi.org/10.3846/16487788.2011.566319.
Published in Issue
Apr 14, 2011
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