Avionics Systems

 

Where Ideas and Technology Meet!
COMMUNICATION INTERFACE UNIT and END CONNECTION UNIT

We are developing flight / ground control and communication systems in the Unmanned Aerial Vehicle, developed with local and national facilities for use in defense systems.

The communication interface unit and terminal unit are equipment that complies with the electrical / mechanical standards of avionics systems, which can differ in their basic functions because of their configuration in different configurations even though they have the same hardware components, which are capable of performing the functions of signal processor, data concentrator and protocol converter.

HAU
  • 2 x Gigabit Ethernet Interface
  • 8 x Fast Ethernet Interface
  • 1 x MIL-STD-1553B Interface
  • 3 x SD Video inputs
  • 8 x RS-422 Interface
  • Ability to Operate in a Temperature Range of -55 °C / +55 °C
  • Self-heating at Low Temperatures
  • H.264 / MPEG-4 Part 10 to Video Compression
  • ESD Protection
  • Compliance with EMI / EMC Tests
  • Ability to Operate in 12V / 36V Voltage Range
  • Protection Against High and Reverse Voltage
  • Configurable via Ethernet
  • Error Logging Feature
  • Can be used as L2 Managed Switch
  • Static Routing
  • Protocol Conversion
  • Video Switching
UBB
  • 24 x (± 10V) Analog Input
  • 4 x (± 40V) Analog Input
  • 10 x (± 10V) Analog Output
  • 16 x Digital Input
  • 16 x Digital Output
  • 8 x GPIO
  • 1 x Thermocouple
  • 1 x Frequency Input
  • 2 x PWM Output
  • 5 x Constant Voltage Supply (CVS)
  • 5 x Constant Current Source (CCS)
  • 1 x RS232 Interface
  • 4 x RS422 Interface
  • 4 x RS485 Interface
  • 2 x MIL-STD-1553B Interface
  • Configurable via Serial Channel
  • Wide operating temperature in the range of -55 °C / +55 °C
  • Self-heating at Low Temperatures
  • ESD Protection
  • Compliance with EMI / EMC Tests
  • Ability to Operate in 12V / 36V Voltage Range
  • Protection Against High and Reverse Voltage
Standards Supported By HAU-UBB
  • MIL-STD-1553B
  • TIA/EIA-232E
  • ANSI/TIA/EIA-422-A-98
  •  ANSI/TIA/EIA-485-A-98
  • MIL STD 461E RTCA DO-160G
  • MIL STD 704F
  • MIL-STD-810G

Since 2008, Pavotek has been continuing its R&D activities within the scope of unmanned aerial vehicles (UAV) with many outstanding projects support by Pavelsis teams.