eVTOL Propulsion System

about project

The client, a leading manufacturer of eVTOL (Electric Vertical Take-Off and Landing) aircraft that is at a mature stage of development of the aircraft and all on-board systems required support in software development and verification for safety-critical on-board system (DAL A) Propulsion System (PS).

All activities must be performed strictly according to aviation industry standards, particularly DO-178C and DO-331.

Technologies

  1. Embedded Software
  2. C language
  3. MATLAB/Simulink
  4. Vector CAST
  5. Enterprise Architect
  1. Embedded Software
  2. C language
  3. MATLAB/Simulink
  4. Vector CAST
  5. Enterprise Architect

Standarts

  1. DO-178C
  2. DO-331
  3. ARINC 646
  4. ARINC 664
  5. ARINC 825
  6. ARINC 429
  1. DO-178C
  2. DO-331
  3. ARINC 646
  4. ARINC 664
  5. ARINC 825
  6. ARINC 429

Domain knowledge

tasks

01
01

Development and verification of the software for the PS.

02
02

Conduct all development and verification activities in compliance with DO-178C and DO-331 standards.

03
03
03
03
04
04
05
05
06
06
07
07
08
08

Results

Software Development activities:

Software Design Description, Software High-level Requirements, Software Low-level Requirements, Source Code, Integrated Software.

Software Verification activities

Requirements Review, Design Document Review, Source Code Reviewed, Test Cases and Test Procedures Running using VectorCAST tool and Simulink Test.

Adherence to standards

All development and verification activities are fully compliant with DO-178C, DO-331 and company standards and methods.

process

review

contacts

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IEC 62304
ISO 13485
ISO 9001
APR-4761
APR-4754A
DO-254
DO-248
DO-178
DO-330
DO-297
DO-331
DO-332
DO-333
Compliance