SIMULASI GERAK DAN ANALISIS KESTABILAN KOPLING INERSIA WAHANA DIRGANTARA DENGAN BENTUK BADAN RAMPING

Authors

  • Hari Muhammad Kelompok Keahlian Fisika Terbang, Fakultas Teknik Mesin dan Dirgantara, Institut Teknologi Bandung
  • Hilman Samputra Kelompok Keahlian Fisika Terbang, Fakultas Teknik Mesin dan Dirgantara, Institut Teknologi Bandung
  • Yazdi I. Jenie Kelompok Keahlian Fisika Terbang, Fakultas Teknik Mesin dan Dirgantara, Institut Teknologi Bandung
  • Javensius Sembiring Kelompok Keahlian Fisika Terbang, Fakultas Teknik Mesin dan Dirgantara, Institut Teknologi Bandung

Keywords:

Inertia coupling, Stability analysis, Slender body, Flight simulation

Abstract

Inertia coupling is a motion phenomenon of a high-speed airplane having slender body and low aspect ratio. This inertia coupling happens when the aircraft performs a roll manoeuvre motion with a high roll rate. This paper will discuss the derivation of inertia coupling equations of motion, modelling equations of motion in the Matlab/Simulink software, simulating the dynamics motion, and analyzing the stability of the inertia coupling. Numerical simulation and stability analysis of the inertia coupling for a fighter aircraft will be presented in this paper.

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Published

08-02-2012

How to Cite

Muhammad, H., Samputra, H., Jenie, Y. I., & Sembiring, J. (2012). SIMULASI GERAK DAN ANALISIS KESTABILAN KOPLING INERSIA WAHANA DIRGANTARA DENGAN BENTUK BADAN RAMPING. Indonesian Journal of Aerospace, 9(1 Juni), 28–40. Retrieved from https://ejournal.brin.go.id/ijoa/article/view/12401

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