Further investigations on newton-raphson methods in aircraft trim

Millidere M., Karaman U., Ballı H., Çimen T.

AIAA Science and Technology Forum and Exposition, AIAA SciTech Forum 2021, Virtual, Online, 11 - 15 Ocak 2021, ss.1-30 identifier

  • Yayın Türü: Bildiri / Tam Metin Bildiri
  • Cilt numarası:
  • Basıldığı Şehir: Virtual, Online
  • Sayfa Sayıları: ss.1-30
  • Orta Doğu Teknik Üniversitesi Adresli: Evet

Özet

© 2021, American Institute of Aeronautics and Astronautics Inc, AIAA. All Rights Reserved.This paper is a follow-up on a prior work on aircraft trim using Newton-Raphson methods for steady and level flight, climb or descent, steady turn, and pull-up or push-over flight conditions. The current study extends this work to steady climbing/descending turn, crosswind landing, steady heading steady sideslip, aileron roll, and barrel roll trim conditions based on classical and Line-Search Newton Raphson methods.