Avionics Hardware Design

Service 03 · Avionics hardware

Airborne electronics, designed for certification.

Flight-control computers, mission computers and FPGA avionics cards, taken from requirements to qualified prototype under DO-254 design assurance and DO-160 environmental requirements.

SCROLL
DO-254Design assurance processes
DO-160Environmental conditions
ARP4754ASystem development
1553·429MIL-STD-1553 · ARINC 429 · AFDX
MILMIL-STD-810 / 461 / 704
01 · Inside a line-replaceable unit

A mission computer, built card by card.

A rugged conduction-cooled chassis, a backplane, processor, FPGA I/O and power cards, sealed with MIL-DTL-38999 connectors. Watch it assemble.

LRU ASSEMBLY · ILLUSTRATIVE
02 · Avionics data buses · Interactive

Deterministic, redundant, certifiable.

We implement avionics bus interfaces in FPGA and on board: MIL-STD-1553B with dual redundancy, ARINC 429 point-to-multipoint links and AFDX switched Ethernet.

BUS SIMULATION · ILLUSTRATIVE
03 · Design assurance

DO-254 from day one.

Certification is designed in, not added at the end. Every requirement traces through design and verification to evidence your certification authority can review.

  • Plans: PHAC, hardware design, validation, verification, configuration and process assurance
  • Requirements captured, validated and traced to design and test
  • Design reviews at conceptual, detailed and implementation stages
  • Verification with coverage, independence and elemental analysis for DAL A/B
  • Environmental qualification to DO-160 and MIL-STD-810
04 · Qualification

Built to survive the flight envelope.

We design for the environment from the start, with thermal, vibration, power and EMC margins verified by analysis and in test.

QUALIFICATION PROFILES · ILLUSTRATIVE
Illuminated aircraft cockpit at nightFlight deck
Electronics you can certifyHardware for manned aircraft, helicopters and UAVs.
Digital cockpit gaugesDisplays & I/O
Interfaces to the whole aircraftDiscrete, analog, serial and bus I/O.
05 · What we deliver

From requirements to qualified prototype.

Flight-control & mission computers

Redundant processing, rugged conduction-cooled chassis and deterministic I/O for flight-critical functions.

FPGA-based avionics cards

DO-254-ready FPGA designs for I/O concentration, sensor processing, video and graphics.

Bus interfaces

MIL-STD-1553B BC/RT/MT, ARINC 429, AFDX / ARINC 664, CAN and RS-422 on board and in FPGA.

Power & I/O boards

28 V avionics power conditioning to MIL-STD-704 and DO-160, discrete and analog I/O.

Certification evidence

Plans, requirements, traceability, reviews and verification records for your certification authority.

Test & qualification

Test equipment, hardware-in-the-loop benches and management of environmental and EMC test campaigns.

DO-254 DAL A–EDO-160GARP4754AMIL-STD-810HMIL-STD-461GMIL-STD-704FMIL-STD-1553BARINC 429AFDX · ARINC 664MIL-DTL-38999
Start your avionics programme

Bring us your requirements.

We will propose an architecture, a certification approach and a schedule matched to your design assurance level.

  • DO-254 design assurance processes
  • Rugged, conduction-cooled hardware
  • Bus interfaces in FPGA and on board
  • Teknopark İstanbul