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This content describes about the life cycle hardware design of Avionics. Explain about various phases of the design cycles like requirement capture, Design,Testing, Verification and Validation and Certification.Most of the life cycle talks about how a design needs to be comply with the aircraft standards such as DO-254, DO160G.The content is explained to be understandable by a layman and for more reference and understanding please refer the above mentioned standards.

Produktbeschreibung
This content describes about the life cycle hardware design of Avionics. Explain about various phases of the design cycles like requirement capture, Design,Testing, Verification and Validation and Certification.Most of the life cycle talks about how a design needs to be comply with the aircraft standards such as DO-254, DO160G.The content is explained to be understandable by a layman and for more reference and understanding please refer the above mentioned standards.
Autorenporträt
I am Sunilkumar Gopakumar working as a Sr Engineering Manager for Collins Aerospace Systems Safety department. I have more than 12+ years of experience in working for Embedded Systems and Hardware development Projects for Avionics.