Open AccessINTEGRATION OF THE MEASURED ALTITUDE-SPEED PERFORMANCES IN THE SYSTEM
Author(s) -
А. И. Пономарев,
Mikhail Yu. Sorokin
Publication year - 2021
Publication title -
avtomatizaciâ processov upravleniâ
Language(s) - English
Resource type - Journals
ISSN - 1991-2927
DOI - 10.35752/1991-2927-2021-2-64-18-22
Subject(s) - aircrew , altitude (triangle) , aerospace engineering , aerodynamics , reliability (semiconductor) , computer science , measure (data warehouse) , density of air , simulation , automotive engineering , engineering , meteorology , physics , mathematics , power (physics) , geometry , quantum mechanics , database
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 onboard 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.