Constrained control of helicopter vibration to reduce motion blur

Oktay T., Celık H., Türkmen I.

AIRCRAFT ENGINEERING AND AEROSPACE TECHNOLOGY, cilt.90, ss.1326-1336, 2018 (SCI-Expanded) identifier identifier

  • Yayın Türü: Makale / Tam Makale
  • Cilt numarası: 90
  • Basım Tarihi: 2018
  • Doi Numarası: 10.1108/aeat-02-2017-0068
  • Dergi Adı: AIRCRAFT ENGINEERING AND AEROSPACE TECHNOLOGY
  • Derginin Tarandığı İndeksler: Science Citation Index Expanded (SCI-EXPANDED), Scopus
  • Sayfa Sayıları: ss.1326-1336
  • Anahtar Kelimeler: Blur kernel, Constrained control, Helicopter vibration, Motion blur, INFINITY CONTROL DESIGN, FLIGHT, IMAGE, OPTIMIZATION, ALGORITHM
  • Erciyes Üniversitesi Adresli: Evet

Özet

Purpose - The purpose of this paper is to examine the success of constrained control on reducing motion blur which occurs as a result of helicopter vibration.