Jurnal Teknologi Dirgantara
Vol 9, No. 1 Juni (2011)

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

Hari Muhammad (Fakultas Teknik Mesin dan Dirgantara Institut Teknologi Bandung)
Hilman Samputra (Fakultas Teknik Mesin dan Dirgantara Institut Teknologi Bandung)
Yazdi I. Jenie (Fakultas Teknik Mesin dan Dirgantara Institut Teknologi Bandung)
Javensius Sembiring (Fakultas Teknik Mesin dan Dirgantara Institut Teknologi Bandung)



Article Info

Publish Date
08 Feb 2012

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. Keywords:Inertia coupling, Stability analysis, Flight simulation, Slender body

Copyrights © 2011






Journal Info

Abbrev

jurnal_tekgan

Publisher

Subject

Aerospace Engineering Chemical Engineering, Chemistry & Bioengineering Computer Science & IT Mechanical Engineering Physics

Description

Jurnal Teknologi Dirgantara (Journal of Aerospace Technology) is an Indonesian accredited scientific publication that covers topics of Rocket, satellite, and aeronautics technology, as well as a spin-off from aerospace technology, such as aerodynamics, astronautics, aerospace structure, power and ...