PIL simulations of an FWUAV under windy conditions

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Atıf İçin Kopyala

Ulker H., Baykara C., Ozsoy C.

AIRCRAFT ENGINEERING AND AEROSPACE TECHNOLOGY, cilt.90, sa.2, ss.461-470, 2018 (SCI-Expanded)

• Yayın Türü: Makale / Tam Makale
• Cilt numarası: 90 Sayı: 2
• Basım Tarihi: 2018
• Doi Numarası: 10.1108/aeat-06-2016-0096
• Dergi Adı: AIRCRAFT ENGINEERING AND AEROSPACE TECHNOLOGY
• Derginin Tarandığı İndeksler: Science Citation Index Expanded (SCI-EXPANDED), Scopus
• Sayfa Sayıları: ss.461-470
• İstanbul Teknik Üniversitesi Adresli: Evet

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.