WHAT WE DO
Based on our experience in the development of electrical systems for the next-corps level unmanned aerial vehicle (UAV-II) and small unmanned aerial vehicle (certifiers), we have conducted all design and manufacturing of electrical system architecture, power load analysis, electrical system component design and manufacturing, as well as in-house testing and evaluation.
Overview
Power load analysis is performed by designing the electrical system architecture for the entire aircraft.
Architecture design
Design an appropriate electrical system architecture for aircrafts 01Power load analysis
Analyze the load and design capacity requirements for all aircraft components 02Electrical system
Design and manufacture/verify the entire electrical system 03Redundancy
Redundant design of essential equipment considering aircraft safety 04
Configuration
Provide the highest safety with power distribution and
control technology, aircraft electrical wiring and protection
circuit design technology, and redundant algorithms according
to operating conditions.
