IDENTIFICATION AND ASSESSMENT OF THE AIRCRAFT FUNCTIONAL SYSTEMS IN THE FLIGHT SAFETY MANAGEMENT SYSTEMS

Abstract

The article discusses issues related to determining the technical states of aircraft functional systems (FS). Mathematical formulas are given for expressing the relationship between the main parameters characterizing the model.

Keywords

• воздушное судно
• функциональные системы
• функциональный отказ
• потребляющий элемент