DETERMINING THE KINEMATIC PARAMETERS OF AIRCRAFT MOTION ON THE BASIS OF TELEMETRIC MEASUREMENT FILTRATION
The problem of determining kinematic parameters of aircraft motion at the boost phase is characterized by a number of peculiarities, connected with the limited amount of measurement data for individual flight segments. To filtrate the test array of telemetry data being investigated, that contains the discrete values of apparent velocity, a filtering algorithm on the basis of the discrete wavelet transformation has been developed. We propose the technique of identifying the parameters of aircraft motion based on the telemetric measurements results in the absence of a priori data about statistical characteristics of measurement errors and estimated parameters.