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Supersonic UAV Flight Control System
The UKS device manages the flight control system of the Supersonic Aerial Vehicle. It acts as an electrical bridge between sensors and equipment that assist flight control. For that purpose, UKS, which has different types of inputs and outputs, performs flight control with the information it receives from sensors and equipment. Also, it can record all flight data with its 1 GB NVM.
CPU Block
- Input Voltage 14-18V 20A (maximum)
- 1 x 1 Gigabit Ethernet
- 1 x 10/100 Mbps Fast Ethernet
- 6 x Analog Input Channel between +-10V
- 1 x 7V 5A Current Protected 5W Power Output
- 1 x RS422
- 1 x RS485
- 3 x RS232
- 1 x UART
- 1 x USB OTG
- 1 x USB
- 2 x 5V PWM Output
- 2 x CANBUS
- 6 x 5A Current Protected Battery Voltage Output
- 3 x 10A Current Protected Battery Voltage Output
- 1 x 15A Current Protected Battery Voltage Output
- Feature of Reading Input Current and Voltage Information
FPGA Block
- Input Voltage 14-18V 5A (maximum)
- 16 x Analog Input Channel between +-10V
- 1 x Analog Input Channel between +-10V
- 1 x 7V 5A Current Protected 5W Power Output
- 1 x 5V PWM Output
- 1 x CANBUS
- 1 GB Storage for Log Recording
- Feature of Reading Input Current and Voltage Information
CPU-FPGA Connection Interfaces
- 1 x UART
- 1 x Mutual Life Signal
