Design of MPCs for a fixed wing UAV

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Atıf İçin Kopyala

Ulker H., Baykara C., Ozsoy C.

AIRCRAFT ENGINEERING AND AEROSPACE TECHNOLOGY, cilt.89, sa.6, ss.893-901, 2017 (SCI-Expanded)

• Yayın Türü: Makale / Tam Makale
• Cilt numarası: 89 Sayı: 6
• Basım Tarihi: 2017
• Doi Numarası: 10.1108/aeat-08-2015-0198
• Dergi Adı: AIRCRAFT ENGINEERING AND AEROSPACE TECHNOLOGY
• Derginin Tarandığı İndeksler: Science Citation Index Expanded (SCI-EXPANDED), Scopus
• Sayfa Sayıları: ss.893-901
• İstanbul Teknik Üniversitesi Adresli: Evet

Özet

Purpose - The purpose of the paper is to examine a fixed wing unmanned aerial vehicle (UAV) as it undergoes five flight scenarios under straight and level, level climb, level turn, climbing turn and level steady heading sideslip conditions in a desired and controlled manner using constrained multi input multi output (MIMO) model predictive controllers (MPCs).