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http://dx.doi.org/10.12673/jant.2022.26.2.99

A Study on the Design and Rectification Method of a KW class Power Converter Unit for an Aircraft Mounted Guided Missile  

Kim, Hyung-Jae (PGM1 R&D Lab, LIG Nex1)
Jung, Jae-Won (PGM1 R&D Lab, LIG Nex1)
Lee, Dong-Hyeon (PGM1 R&D Lab, LIG Nex1)
Kim, Gil-Hoon (PGM1 R&D Lab, LIG Nex1)
Moon, Mi-Youn (The 3rd Missile Systems PMO, Agency For Defense Development)
Publication Information
Journal of Advanced Navigation Technology / v.26, no.2, 2022 , pp. 99-104 More about this Journal
Abstract
Recently, the domestic demand for weapon systems based on aircraft platforms is gradually increasing. In particular, the demand for effective precision guided missile(PGM) which cruises for several hundred kilometers after launch to strike the ground target is rising drastically, but it is in the early stages of development, and research based on it are limited. This paper is a study on the power converter unit(PCU) within PGM which is mounted on an aircraft platform based on MIL-STD-1760, which is an interface between an aircraft and PGM. We investigated the electrical properties and structure of the umbilical connector, and the aircraft/store electrical interconnection system. Also, the focus on the design specifications of the PCU that supplies power were described. This result 3 phase AC input, which is the state for the guided simulation power supply in the state of being mounted on an aircraft that rectification method with power factor correction(PFC) compared to bridge rectifier circuit. In the future, it may be used as a basis for power supply design on aircraft mounted weapon systems.
Keywords
Bridge rectifier; Power converter unit; Power factor correction; Umbilical; Weapon systems;
Citations & Related Records
Times Cited By KSCI : 1  (Citation Analysis)
연도 인용수 순위
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