Low cost modular architecture of piloting and aerodyne operating with high level of security
A module structure, the technology of the aircraft, the redundancy in the hardware is used for data error detection, reliability/availability analysis, instruments, etc., to achieve the effect of convenient fault detection and repair operations
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[0029] The structure of the airborne electronic equipment components shown in Figure 1 makes it possible to complete the automatic driving of the aircraft, provide stall protection, and complete the data collection and centralized maintenance of these equipment components. To this end, it contains five key display devices 3-7; two housing units 1, 2 housing two identical modular processing components IFC1 and IFC2 (Integrated Flight Box); two main reference systems 8, 9, They are the sensors that transmit critical data, and each includes, for example, an AHRS (Attitude Orientation Reference System) attitude unit and an ADC (Air Data Computer) system for collecting and processing data related to the air outside the cabin, enabling short-term Acquisition of flight parameters; two engine parameter measuring devices FADEC1 and FADEC2 (full authority digital engine computer) 10, 11; a set of actuators 12 and non-critical sensors for transmission of non-critical data such as sensors,...
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