MFCS is a flight control computer designed for use in unmanned aerial vehicles. MFCS’s architecture has been designed in line with the principle of controlling all activities of the flight sensors, control surfaces, communication systems and other aircraft subsystems in the aircraft, such as high-level management, control, monitoring and similar activities, by central computers.
• Digitally controlled by vehicle computer
• UAV Management System
• UAV Communication System
• Trip Function and health status
• Reverse Current Protection
• Compact, Lightweight, Low-Cost
• FPGA, Artix7, 250-I/O, 2600-CLB, 33208-Cell, 484-FBGA
• 2x Arm Cortex™-A724x , Arm Cortex™-A53
• 32GB eMMC
• Power Distribution Unit (PDU) Outputs
• Remote Interface Unit (RIU)
• Unmanned Vehicles Control System
• Unmanned Vehicles Communication System
• 10x Analog Input (14-Bit)
• 1x Analog Output (16-Bit)
• 4x RS422
• 6x RS232
• 4x RS485
• 1x Gigabit Ethernet
• 4x 7.4V 6A, Current Protected Power Outputs
• 3x 12V 4A, Current Protected Power Outputs
• 5x 12V 3A, Current Protected Power Output
• 1x USB 2.0
• 1x USB OTG
• 3x CANBUS
• 6x 10/100 Mbps Fast Ethernet
• 1x Gigabit Ethernet
• 1x 28V/GND Discrete Input
• 12x Open/GND Discrete Input
• 8x Open/GND Discrete Output
• 12x PWM Interface 5V /1A
• 2x Frekans Input
• Optional ARINC 429 Interface
• Optional MIL-STD-1553 (BC/RT) Interface
• 1 x Input Supply Voltage:14VDC - 32VDC
• 186x126x76 mm
• 1.4± 0.1 kg
• Operating Temperature: -40°C to +55°C
• Storage Temperature: -55°C to +70°C
• Operating Altitude: 40,000ft
• MIL-STD-810G
• MIL-STD-461G
• MIL-STD-704F
• DO-160G
TRL 7/9
