The algorithm of processing and presenting the digital trajectory data obtained when launching rocket vehicles

This research aims at finding a generalized algorithm suitable for processing and presenting the trajectory digital parameters of consumer onboard navigation equipment which is used in the process of space rocket launches. Processing and analysis of digital telemetric information coming from the onboard equipment during the flight and containing digital frames of trajectory measurements is one of the priority tasks as it is the analysis of the path deviations of the rocket that makes a significant contribution to a complete and informative assessment of the launch results. It is suggested that the generalized processing and presenting algorithm which contains the initial stages of the primary processing (extraction of digital frame structures, extraction of trajectory parameters from the frames, mathematical transformations of extracted parameters)as well as determination of primary and secondary values are necessary for solving the trajectory task and, eventually, forming a unified digital stream for representing trajectory measurements, for obtaining results of processing in graphical representation software.