International Journal of Advances in Computer Science and Its Applications
Author(s) : I.THIRUNAVUKKARASU , CIJI PEARL KURIAN , EDGAR FILIPE FLORA , V. I. GEORGE
This paper encompasses the longitudinal dynamics of a Beechcraft King Air 350 aircraft with atmospheric perturbation. Longitudinal simulations with and without integrator states are also discussed. The Linear Quadratic Regulator (LQR) technique showed robustness and it is possible to correct the error in most of the situations. Matlab- Simulink is used as a tool for simulation work.