UKB-501 Flight Control Computer is designed in order to provide multiple reliable interface options, high processing and performance capability for flight sensors, control surfaces, equipments and other avionics sub-systems.
UKB-501 consists of RTCA DO-178B Level B certifiable BSP and driver software for Green Hills Integrity 178B real-time operating system and RTCA-DO-254 Level B certifiable hardware.
Isolated interface groups, fully redundant power circuits and Built-In-Test capabilities of UKB-501 provide reliable and safe operation during the mission. Rugged, lightweight and conduction-cooled UKB-501 hardware is designed to operate in tough airborne environment.
Important Features
General Specifications
RTCA DO-254 Certifiable Hardware
RTCA DO-178B Certifiable Software
COM Express Form Factor
BSP and Driver Software for Real-Time Operating Systems with Built-In Test Capability
To be used in ANKA-S UAV and other fixed and rotary wing airborne platforms.
Cooling Method: Conduction cooled thru chassis
Technical Specifications
PowerPC Computing Processor
64 MB Boot Flash Memory
RTC/ETC/WDT
Power Specifications
Input : 28 VDC
Power hold-up for short power interrupts
Power Consumption : < 60W
Software Specifications
Operating System: Integrity-178B RTOS
Interfaces
8x OPEN/GND Discrete Input, 8x OPEN/GND Discrete Output
4 x MIL-STD-1553B Interface
13 x RS-422/RS-485 Interface (2400 - 230400 baud rate)
3 x CAN 2.0 A&B CANBus Interface (100Kbit/sec - 1Mbit/sec)
8 Rx and 4 Tx ARINC 429 Interface (12.5 Kbps - 100 Kbps)
4x software configurable Synchronous / Asynchronous RS-422 Interface (2400 - 230400 Baud Rate)
1 x 10/100 Ethernet Interface
1x 10/100/1000 Ethernet Interface
Qualifications
MIL-STD-704
MIL-STD-810 / DO-160
MIL-STD-461
Physical Specifications
Dimensions: 290mm (W) X 81.7mm (L) X 223mm (H)
Weight : < 4.5kg
