A solution to build a simulation environment to synthesize data to determine the limited angle of attack parameters of the su-27 aircraft
102 viewsDOI:
https://doi.org/10.54939/1859-1043.j.mst.CAPITI.2024.140-146Keywords:
Allowable limit angle of attack; COC-2-1 system; Su-27.Abstract
This article presents a solution to build a simulation environment to synthesize data to determine the allowable limit angle of attack parameters of the Su-27 aircraft. This parameter is determined to serve the process of researching and designing a limited signals computer of the Su-27 aircraft (under the information security conditions of the aircraft manufacturer, there are no aerodynamic parameters). The solution is simple and easy to apply to determine the limited angle of attack for Su-27 aircraft as well as other types of aircraft.
References
[1]. Институт транспорта и связи “Oсновы аэродинамики и динамики полета” Рига, (2010).
[2]. И. С. Зегжда, С. Г. Бурлуцкий, А. М. Павлов “Pасчет летных и маневренных характеристик самолета” Методические указания к выполнению домашнего задания Санкт – Петербург, (2015).
[3]. “Сиcтeма Oграничительных Cигналов COC-2-1” Pуководство по Tехнитекой Эксплуатации, (1991).
