Aerospace Instrument-Making Annotation << Back Algorithm for calculating actual values of aircraft aerodynamic parameters A.I. Oleynik The synthesis of optimum estimation algorithm for determination of static and total pressure local values, and aerodynamic angles based on pressure values measured in specific points of aircraft pressure field is under consideration. The second stage is connected with revaluation of local flight configuration values into aerodynamic parameter ideal values. Key words: aerodynamic parameters, incidence angle, gliding angle, optimum filtering, air pressure, sensor errors. Контактная информация: E-mail: aoleynik@hse.ru. P. 3-10