Constrained control of helicopter vibration to reduce motion blur

Oktay T., Celık H., Türkmen I.

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

  • Publication Type: Article / Article
  • Volume: 90
  • Publication Date: 2018
  • Doi Number: 10.1108/aeat-02-2017-0068
  • Journal Name: AIRCRAFT ENGINEERING AND AEROSPACE TECHNOLOGY
  • Journal Indexes: Science Citation Index Expanded (SCI-EXPANDED), Scopus
  • Page Numbers: pp.1326-1336
  • Keywords: Blur kernel, Constrained control, Helicopter vibration, Motion blur, INFINITY CONTROL DESIGN, FLIGHT, IMAGE, OPTIMIZATION, ALGORITHM
  • Erciyes University Affiliated: Yes

Abstract

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.