CR9 Integrated Avionics

The product uses a distributed computer to cross-link a variety of airborne electronic sub-systems through a multiplexed data bus. It combines the existing single-function decentralized systems, such as communication stations, radars, navigation equipment, etc., to make overall arrangements to form a multi-functional integrated system, which can realize the functions of information measurement, collection, transmission, processing, monitoring and display, and complete Flight control, engine control, navigation, performance management and other tasks. The CR9 general aviation integrated avionics system has independent intellectual property rights and is installed on manned aircraft through airworthiness certification. It occupies a prominent position in modern aircraft. Together with the aircraft body and engines, it forms a complete aircraft industry chain. The advanced avionics system is an aircraft. The important guarantee of safety, economy and comfort is an important indicator of the advanced degree of aircraft.
Product Features:
1. Flexible, modular system structure
2, clear wireless data / software design
3, double 16 watts, 8.33 kHz, 4 wireless channels
4, double ADHRS, equipped with cross comparison
 5, dual WAAS GPS transceiver support
6, EADI and EHSI integration features
7, dual or triple high resolution display
8, redundant and interchangeable display
9, FMS and GeoFill prediction menu
10. Synthetic (SVS) & Enhanced (EVS) vision system
11. Display maps, charts, FMS, checklists, EVS, SVS, engines, traffic, data transceivers, and lighting systems.
Main Specifications:
System: an integrated cockpit composed of 10.4-inch displays with multiple integrated PFD, MFD, ADAHRS, GPS and VHF functions
Operating system: real-time partition operating system Vxworks65
Bsp driver software: including SDRAM, NORFLASH, NVRAM, I2C, SPI, EPIC, PCIe, Ethernet, UART0/1, CAN driver software
Hardware platform: P2010 processor based on e500 core architecture, clocked at 1GHz
Interface display: including the display and control of parameters such as heading attitude, heading, airspeed, navigation, engine data management, flight plan management failure warning, etc.
Display size: 10.4 inches; power supply: +28V
Communication method: Ethernet communication
Display module volume: a single volume is less than 420mm×340×65mm


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