Simulation of aircraft control using bond graph techniques and matlab simulink software

Abstract EN

To develop the nonlinear transformer that is required for particular implementation of a complex aircraft control system.

Aircraft longitudinal and lateral motions are presented by studying and analyzing the aircraft dynamics.

The equations of motion are covered both forces and moments exerted on the aircraft using Newton's second law with the assumption that at each equation the aircraft is regarded as a rigid body.

Six equations were classified, three equations for the longitudinal motion and three equations for the lateral motion.

The matrix for the differential equations vectors for each force and moment were found with the aid of the computer aided modern bond graph program (CAMP-G) including symbolic manipulation.

MATLAB / SIMULINK offered additional simulation capability.