Constrained control of helicopter vibration to reduce motion blur
AIRCRAFT ENGINEERING AND AEROSPACE TECHNOLOGY, cilt.90, ss.1326-1336, 2018 (SCI-Expanded, Scopus)
- 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
- 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.