Nonlinear Simulation of Aircraft Longitudinal Flight Dynamics

Tariq O. Mohammed; Xiang Jin Wu; Dao Chun Li

doi:10.4028/www.scientific.net/AMM.444-445.753

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HomeApplied Mechanics and MaterialsApplied Mechanics and Materials Vols. 444-445Nonlinear Simulation of Aircraft Longitudinal...

Nonlinear Simulation of Aircraft Longitudinal Flight Dynamics

Abstract:

The purpose of this paper is to simulate flight path of Boeing-747 for longitudinal motion at selected flight conditions using 6 DoF (Degrees of freedom) nonlinear equations with MATLAB and SIMULINK. The equations are solved to compute the flight path within 100 seconds of Boeing 747 at three flight conditions, for cruise flight with different Mach numbers at same altitudes, and then Mach number at high altitude with MATLAB programming (ode45). Simulation results for different conditions are presented and analyzed.

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Periodical:

Applied Mechanics and Materials (Volumes 444-445)

Pages:

753-758

DOI:

https://doi.org/10.4028/www.scientific.net/AMM.444-445.753

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Online since:

October 2013

Authors:

Tariq O. Mohammed, Xiang Jin Wu, Dao Chun Li

Keywords:

Longitudinal Dynamics, Nonlinear Equations, Simulation

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