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http://dx.doi.org/10.5515/KJKIEES.2018.29.8.583

Development and Verification of Aircraft Controller and Transceiver Considering Lightning Induced Transient Susceptibility  

Seo, Jung-Won (Satellite Datalink Team, Hanwha Systems)
Park, Jae-Soo (Satellite Datalink Team, Hanwha Systems)
Yoon, Chang-Bae (Satellite Datalink Team, Hanwha Systems)
Hong, Su-Woon (Satellite Datalink Team, Hanwha Systems)
Jung, Byoung-Koo (Satellite Datalink Team, Hanwha Systems)
Shin, Young-Jun (Agency for Defense Development)
Ha, Jung-Whan (Danam Systems)
Publication Information
The Journal of Korean Institute of Electromagnetic Engineering and Science / v.29, no.8, 2018 , pp. 583-593 More about this Journal
Abstract
Lightning causes physical damage to aircraft, such as melting, burning and arcing, and magnetic field that occurs on the aircraft's outer body during the penetration of a lightning stroke causes voltage and current transients in the electronics and wiring within the aircraft. This effect will cause induced lightning strikes in the aircraft's internal airborne electronic systems, preventing safe flight. This paper introduces protection circuit design techniques, and the test results that meet the requirements for certification of criteria.
Keywords
Lightning Induced Transient Susceptibility; DO-160; Aircraft; Controller; Transceiver; Airworthiness;
Citations & Related Records
Times Cited By KSCI : 3  (Citation Analysis)
연도 인용수 순위
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