Atıf İçin Kopyala
Koç İ. M., FRANKO S., Ozsoy C.
AIRCRAFT ENGINEERING AND AEROSPACE TECHNOLOGY, cilt.88, sa.6, ss.810-817, 2016 (SCI-Expanded)
-
Yayın Türü:
Makale / Tam Makale
-
Cilt numarası:
88
Sayı:
6
-
Basım Tarihi:
2016
-
Doi Numarası:
10.1108/aeat-01-2015-0004
-
Dergi Adı:
AIRCRAFT ENGINEERING AND AEROSPACE TECHNOLOGY
-
Derginin Tarandığı İndeksler:
Science Citation Index Expanded (SCI-EXPANDED), Scopus
-
Sayfa Sayıları:
ss.810-817
-
Anahtar Kelimeler:
Model predictive control, Autonomous vehicle, Helicopter control, Linear quadratic controller, Velocity control
-
İstanbul Teknik Üniversitesi Adresli:
Evet
Özet
Purpose - The purpose of this paper is to investigate the stability of a small scale six-degree-of-freedom nonlinear helicopter model at translator velocities and angular displacements while it is transiting to hover with different initial conditions.