Non-linear simulation of controller for longitudinal control augmentation system of F-16 using numerical approach

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contributor.author Rachman, Endri en_US
contributor.author Jaam, Jihad M. en_US
contributor.author Hasnah, Ahmad en_US
date.accessioned 2009-12-30T07:32:27Z en_US
date.available 2009-12-30T07:32:27Z en_US
date.issued 2003-09-25 en_US
identifier.citation Endri Rachman, Jihad M Jaam, Ahmad M Hasnah, Non-linear simulation of controller for longitudinal control augmentation system of F-16 using numerical approach, Information Sciences, Volume 164, Issues 1–4, 2 August 2004, Pages 47-60 en_US
identifier.uri http://dx.doi.org/10.1016/j.ins.2003.09.013 en_US
identifier.uri http://hdl.handle.net/10576/10581 en_US
description.abstract The non-linear simulation of controller for automatic flight control system is an essential part of the complete control design process. After using the linear approach in the design and simulation of the controller (control laws), it is important to simulate the controller on the non-linear real aircraft model. This simulation allows us to evaluate its functional performance during the real-time flight on the computer. The results of that process are used to determine whether the designed controller meets the design requirement and objective or not. The paper deals with application of numerical method fourth-order Runge–Kutta to simulate the function of the longitudinal-CAS controller that is embedded into the non-linear, six degree of freedom model of fighter F-16. A computer program is made to implement the numerical approach and to illustrate the result of that simulation on the computer. en_US
language.iso en en_US
publisher Elsevier Inc en
subject Numerical method en_US
subject Non-linear simulation en_US
subject Control augmentation system en_US
title Non-linear simulation of controller for longitudinal control augmentation system of F-16 using numerical approach en_US
type Article en_US


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