Method of expansion of a range of measurement of aerodynamic parameters of flight of a maneuvering plane

In the work the author considers ways and algorithms of definition of aerodynamic parameters of flight of a maneuvering plane on any angles of attack and sliding, khe given method assumes to measure a field of pressure of the plane by means of multi-hole receivers of pressure and processing of the received information with optimum algorithms, on the basis of the developed mathematical model of pressure.