ISSN 1991-2927
 

ACP № 3 (65) 2021

Author: "Artem Igorevich Ponomarev,"

Artem Igorevich Ponomarev,, graduated from Ulyanovsk State Technical University with a degree in Instrumentation; Postgraduate Student at the Department of Measuring and Computing Systems of UlSTU; his research interests are in the field of designing aerometric equipment. e-mail: artem_lsp@mail.ruA.I. Ponomarev,

Mikhail Iurievich Sorokin, Candidate of Sciences in Engineering; graduated from UlSTU with a degree in Aviation Devices and Measuring-Calculating Complexes; Associate Professor at the Department of Measuring and Computing Systems of UlSTU; his research interests are in the field of aerometric equipment development. e-mail: minich80@mail.ruM.I. Sorokin

Integration of the measured altitude-speed performances in the system64_3.pdf

The air data system used by modern aircrafts is a soft hardware designed to measure, compute, and display the altitude-speed performances as well as other parameters such as air temperature, angles of attack and slip; and to provide to aircrew and consumers (various on-board systems) with this information. The speed and altitude are one of the most important flight parameters of an aircraft. The operating principle of modern on- board equipment for measuring the aircraft movement parameters while in flight is based on an aerometric method. This article deals with a method for increasing the accuracy and the reliability of aerodynamic angle-of-attack measurements.

Measurement, pressure, pressure probe, sensor, air data, angle of attack, aircraft, mathematical model, air data system.

2021_ 2

Sections: Information systems

Subjects: Information systems.



© FRPC JSC 'RPA 'Mars', 2009-2021 The web-site runs on Joomla!