IMPACT OF AN UNDERSLUNG LOAD ON A HELICOPTER CONTROLLABILITY
This article is aimed at finding the causes of controllability variations of a helicopter while transporting sling load.The maximum angular acceleration taken by the helicopter at similar controller displacement at different flight speeds was taken as a quantity characteristic of controllability eff...
| Автори: | , , |
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| Формат: | Стаття |
| Мова: | Russian |
| Опубліковано: |
Moscow State Technical University of Civil Aviation
2017-01-01
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| Серія: | Научный вестник МГТУ ГА |
| Предмети: | |
| Онлайн доступ: | https://avia.mstuca.ru/jour/article/view/980 |