A post-flight analyses technique to support flight tests of light aeroplanes

Аuthors

Baranov V. N.^*, Zaw L. O.^**

Moscow Aviation Institute (National Research University), 4, Volokolamskoe shosse, Moscow, А-80, GSP-3, 125993, Russia

*e-mail: vnb36@mail.ru
**e-mail: zaw.lin@mail.ru

Abstract

One of actual contemporary scientific and engineering problems is design of light airplanes intended for monitoring of natural and technogeneous disasters. Flight test is very important step in design process for any aircraft including light one. Aerodynamical and other characteristics are revealed and refined by means of flight test. Proposed two step scheme for solving the problem on the basis of preliminary processing of transients and the use of the method of least squares, follow by the final processing of information using the Kalman filter

Keywords:

light airplane, aerodynamic coefficient, transient process, filter Kalman