Hovering stability of a model helicopter


Koç İ. M., FRANKO S., Ozsoy C.

AIRCRAFT ENGINEERING AND AEROSPACE TECHNOLOGY, cilt.88, sa.6, ss.810-817, 2016 (SCI-Expanded) identifier identifier

  • 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.