DEVELOPER AND INTEGRATOR OF EMBEDDED SOFTWARE
AND APPLICATIONS

Defibrillator Battery Management Unit software verification, including automated testing and certification documentation (Class III medical device), following IEC 62304 and ISO 13485 standards.

Series of integrations between various laboratory devices and the customer's existing LIS, ensuring seamless communication between the devices and the customer’s software, enhancing data handling, device control, and workflow automation.

Development of a Test Automation Framework (TAF) to automate the testing and verification process for new products.

Development of an automated genotyping software based on electrophoresis data from genetic analyzers.

Development of an AI-driven system to automate urine analysis and livestock management.

Development of lab robot digital-twin to reduce development time, speed up market release, and cut costs by minimizing reliance on physical prototypes.

The client required a safety assessment (ARP4761), the development of plans and standards, requirements engineering (ARP4754A), and software verification for the wing devices control system, the electric flap control system, the aircraft spoiler electric drive, and the electric drive of an aircraft engine reverse device.

eVTOL Platform Software Verification for all on-board systems, adhering to DO-178C and DO-331.

Software development and verification for safety-critical (DAL A) Propulsion System, adhering to DO-178C and DO-331.

eVTOL Flight Control Laws Software Requirements Development, adhering to DO-178C and DO-331.

Software development and verification for an eVTOL safety-critical (DAL A) Flight Control Computer, adhering to DO-178C and DO-331.

Development and verification of software and FPGA for the Multi-Function Air Data System, according to DO-178C, DO-254, and ARP-4754A.

Development and verification of a Multi-Function Display Unit (MDU) according to DO-178C DAL B: writing high/low-level requirements, software development, testing, and refactoring, with the MDU built on the ARINC 661 standard.

Development of software requirements, coding, and integration for Elbit Head-up Display (HUD) according to DO-178C.

Software development and verification for the eVTOL Critical Flight Control Computer, Engine Speed Controller, and Data Concentrator Unit according to DO-178C and ARP-4754A.

The project involved developing key modules for a Flight Management System (FMS), including lateral/vertical navigation, performance optimization, trajectory prediction, and flight planning. The system supports end-to-end flight plans and integrates with RTOS using ARINC 653 API.

Development and verification of an image processing module for an X-ray imaging system.