05.1 - Flight Dynamics and Control (Control & Modelling)
GENERAL APPROACH TO THE ANALYSIS OF THE ASYMMETRICALLY LOADED AIRPLANE FLIGHT LIMITATIONS
P. Stojakovic, Military Technical Institute, Serbia; B. Rasuo, University of Belgrade, Faculty of Mechanical Engineering, Serbia
General approach to the analysis of asymmetrically loaded airplane limitations within the terminal flight phases is presented in this paper. The goal of the analysis is to supplement the flight envelope limitations of the symmetrically loaded airplane, providing thus the increase of the airplane use safety.