MATHEMATICAL MODELS OF CHANNEL AND ACTUAL SPED OF MACH

Abstract

The aim of this article is to explain simulation model with focus on computing flight parameters such as flight height and speed in the programming environment of MATLAB to reader. The article is based on analytical, mathematical and simulation principles. The problem of atmosphere pressure with correspondence to the international standard atmosphere, flight height and speed simulation computing, Mach´s number computing and the dilemma of the impact of angle of attack and angle of yaw on the speed of flight is solved in the article. The effect of interchanging real and standard static temperature on computing the flight height as well as the matter of air pressure, air temperature and air density changes inflicted by weather alternation are considered in the article.