59324

Автор(ы): 

Автор(ов): 

5

Параметры публикации

Тип публикации: 

Доклад

Название: 

Development of a Laboratory Stand for Research of UAV Aeromechanics and Flight Dynamics

Электронная публикация: 

Да

ISBN/ISSN: 

ISBN:978-1-7281-1094-3

DOI: 

10.1109/MLSD49919.2020.9247715

Наименование конференции: 

  • 2020 13th International Conference "Management of Large-Scale System Development" (MLSD)

Наименование источника: 

  • Proceedings of the 13th International Conference "Management of Large-Scale System Development" (MLSD)

Город: 

  • NY

Издательство: 

  • IEEE (Catalog Number CFP20GAE-ART)

Год издания: 

2020

Страницы: 

1-5
Аннотация
At all stages of the life cycle of unmanned aerial vehicles (UAVs), there is a need for experimental studies of their characteristics. In part, experimental studies of this kind could be performed on installations such as traditional wind tunnels. However, in existing wind tunnels, it is not possible to regulate the air flow speed and study the influence of the aircraft's center of mass position, as is required for evaluating the flight dynamics of modern UAVs. We present a fundamentally new concept of the laboratory stand and methodology for research of UAV aeromechanics and control problems. Results of research of aerodynamic characteristics for several UAVs are given.

Библиографическая ссылка: 

Легович Ю.С., Миодушевский П.В., Миодушевский А.П., Гончаренко В.И., Диане С.А. Development of a Laboratory Stand for Research of UAV Aeromechanics and Flight Dynamics / Proceedings of the 13th International Conference "Management of Large-Scale System Development" (MLSD). NY: IEEE (Catalog Number CFP20GAE-ART), 2020. С. 1-5.