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 İndekslerine Giren Dergi) identifier identifier

  • Cilt numarası: 90
  • Basım Tarihi: 2018
  • Doi Numarası: 10.1108/aeat-02-2017-0068
  • Dergi Adı: AIRCRAFT ENGINEERING AND AEROSPACE TECHNOLOGY
  • Sayfa Sayıları: ss.1326-1336

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.