Suscripción a Biblioteca: Guest

PROTOTYPING THE AERO-INERTIAL SYSTEM FOR MEASURING FLIGHT AIR PARAMETERS IN THE T-105 WIND TUNNEL

Volumen 51, Edición 3, 2020, pp. 297-304
DOI: 10.1615/TsAGISciJ.2020036036
Get accessGet access

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.

REFERENCIAS
  1. Alekseev, N.V., Kravtsov, V.G., Nazarov, O.I., Pankratov, A.K., Vozhdaev, E.S., Vyalkov, A.V., Golovkin, M.A., and Efremov, A.A., The New Generation Systems of Measurements of Flight Parameters, Aviakosmich. Priborost. (Aerosp. Instrum. Making), vol. 8, pp. 31-36, 2003.

  2. Golovkin, M.A., Efremov, A.A., and Leontiev, V.A., The Documental on History of Development of TsAGI Investigations on Helicopters and Spin of Airplanes, Moscow, Russia: Izdatelstvo TsAGI, 2017.

  3. Golovkin, M.A., Efremov, A.A., and Sysoev, V.V., Aerodynamic Layout and Algorithm of a Prospective All-Aspect Air Pressure Probe, Datch. Syst. (Sens. Syst.), vol. 10, pp. 18-26, 2018.

  4. Vyalkov, A.A. and Vyalkov, A.V., Digital Pressure Transducers KDC-24, in Proc. of 2nd Sector-Wide Science-Technical Conference on Measurements Technology and Metrology for Investigating Aircraft (KIMILA-2016), pp. 79-89, 2016.

  5. Vyalkov, A.V., Modern Spin Experiment, in Proc. of 3rd Sector-Wide Science-Technical Conference on Measurements Technology and Metrology for Investigating Aircraft (KIMILA-2018), Moscow, Russia: TsAGI, pp. 476-494, 2018.

  6. Vyalkov, A.V., Inertial Technology of Wind Tunnel Spin Tests, TsAGI Sci. J., vol. 47, no. 5, pp. 537-552, 2016.

Último edicion

KIRILL IVANOVICH SYPALO−50TH ANNIVERSARY NUMERICAL STUDY OF THE DISTURBANCES GENERATED BY MICROJETS IN A SUPERSONIC FLAT-PLATE BOUNDARY LAYER Andrei Valerievich Novikov, Alexander Vitalyevich Fedorov, Ivan Vladimirovich Egorov, Anton Olegovich Obraz, Nikolay Nikolaevich Semenov ANALYSIS OF THE MOVING DETONATION INTERACTION WITH TURBULENT BOUNDARY LAYERS IN A DUCT ON THE BASIS OF NUMERICAL SIMULATION Vladimir Anatolievich Sabelnikov, Vladimir Viktorovich Vlasenko, Sergey Sergeyevich Molev EXPERIMENTAL STUDY OF COUNTERFLOW BLOWING IN HIGH-SPEED FLOW THROUGH AN ASYMMETRIC SLOT IN THE LEADING EDGE OF A SHARP WEDGE Eduard Borisovich Vasilevskii, Ivan Valeryevich Ezhov, Pavel Vladimirovich Chuvakhov ASYMPTOTIC SOLUTIONS TO HYPERSONIC BOUNDARY LAYER EQUATIONS ON A FLAT WING WITH A POINT OF INFLECTION ON THE LEADING EDGE Georgiy Nikolaevich Dudin, Aleksey Vyacheslavovich Ledovskiy WAVE MODEL OF ORGANIZED STRUCTURES IN A TURBULENT BOUNDARY LAYER ON A PLATE WITH ZERO LONGITUDINAL PRESSURE GRADIENT Vladimir Alekseevich Zharov, Igor Ivanovich Lipatov, Rami Salah Saber Selim NUMERICAL SIMULATION OF THE FLOW AROUND LANDSCAPE FRAGMENTS AND SOLUTION VERIFICATION Viktor Viktorovich Vyshinsky, Koang T'in' Zoan POLYNOMIAL REPRESENTATION OF THERMODYNAMIC PROPERTIES OF COMBINED FUEL SYSTEMS IN RAMJET SIMULATION MODELS Timur Romanovich Zuev, Mikhail Semenovich Tararyshkin A MODEL TEST METHODOLOGY FOR THE INVESTIGATION OF AN ELASTICALLY SCALED MAIN ROTOR Maxim Andreyevich Ledyankin , Sergey Anatolyevich Mikhailov, Dmitry Valeryevich Nedel'ko, Timur Arturovich Agliullin INDEX, VOLUME 51, 2020
Portal Digitalde Biblioteca Digital eLibros Revistas Referencias y Libros de Ponencias Colecciones Precios y Políticas de Suscripcione Begell House Contáctenos Language English 中文 Русский Português German French Spain