PIL simulations of an FWUAV under windy conditions


Ulker H., Baykara C. , Ozsoy C.

AIRCRAFT ENGINEERING AND AEROSPACE TECHNOLOGY, vol.90, no.2, pp.461-470, 2018 (Journal Indexed in SCI) identifier identifier

  • Publication Type: Article / Article
  • Volume: 90 Issue: 2
  • Publication Date: 2018
  • Doi Number: 10.1108/aeat-06-2016-0096
  • Title of Journal : AIRCRAFT ENGINEERING AND AEROSPACE TECHNOLOGY
  • Page Numbers: pp.461-470

Abstract

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.