Justification of thrust vector deflection of twin-engine unmanned aerial vehicle power plants
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 deformacija, polinkio momentai.
First published online: 14 Apr 2011
Keywords:
unmanned aerial vehicle (UAV), thrust vectors deflection, adverse and recovery momentsHow to Cite
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Copyright (c) 2011 The Author(s). Published by Vilnius Gediminas Technical University.
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Copyright (c) 2011 The Author(s). Published by Vilnius Gediminas Technical University.
License
This work is licensed under a Creative Commons Attribution 4.0 International License.