PIL simulations of an FWUAV under windy conditions


Ulker H., Baykara C. , Ozsoy C.

AIRCRAFT ENGINEERING AND AEROSPACE TECHNOLOGY, cilt.90, ss.461-470, 2018 (SCI İndekslerine Giren Dergi) identifier identifier

  • Cilt numarası: 90 Konu: 2
  • Basım Tarihi: 2018
  • Doi Numarası: 10.1108/aeat-06-2016-0096
  • Dergi Adı: AIRCRAFT ENGINEERING AND AEROSPACE TECHNOLOGY
  • Sayfa Sayıları: ss.461-470

Özet

Purpose A fixed wing unmanned aerial vehicle (FWUAV) is targeted to perform processor in the loop (PIL) simulations for the flight scenarios such as straight and level, level climb, level turn, climbing turn and level steady heading sideslip under windy conditions such as steady wind (SW) and wind gust (WG) in a desired and controlled manner.