Publicado 6 números por año
ISSN Imprimir: 1948-2590
ISSN En Línea: 1948-2604
PROTOTYPING THE AERO-INERTIAL SYSTEM FOR MEASURING FLIGHT AIR PARAMETERS IN THE T-105 WIND TUNNEL
SINOPSIS
This article presents a new approach to creating advanced systems for measuring air flight parameters. The approach was based on real-time integration of aerometric and inertial motion parameters of an aircraft and was aimed at improving the accuracy and reliability of the measurement results for the altitude and speed flight parameters. The integration was carried out using a special Kalman filter, which is called an air inertial filter. Verification of the quality of the integration and assessment of the capabilities of promising systems was carried out in the vertical TsAGI T-105 wind tunnel during experimental studies of an air inertial system model.
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