PIL simulations of an FWUAV under windy conditions

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Copy For Citation

Ulker H., Baykara C., Ozsoy C.

AIRCRAFT ENGINEERING AND AEROSPACE TECHNOLOGY, vol.90, no.2, pp.461-470, 2018 (SCI-Expanded)

• Publication Type: Article / Article
• Volume: 90 Issue: 2
• Publication Date: 2018
• Doi Number: 10.1108/aeat-06-2016-0096
• Journal Name: AIRCRAFT ENGINEERING AND AEROSPACE TECHNOLOGY
• Journal Indexes: Science Citation Index Expanded (SCI-EXPANDED), Scopus
• Page Numbers: pp.461-470
• Istanbul Technical University Affiliated: Yes

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.