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) |
1 | Tak-bok Kim, "A case study on MIL-STD-1760E based test bench implementation for aircraft-weapon interface testing" Journal of Advanced Navigation Technology, Vol. 22, No.2, pp.57-63, April, 2018. |
2 | MIL-PRF-21480B : Generator system, electric power 400hertz, alternating current, aircraft; general specification for, U.S. Department of Defense, 22 March 2010. |
3 | Miguel A. Maldonado et al., "Power Management and Distribution System for a More-Electric Aircraft (MADMEL) - Program Status," Inter society Energy Conversion Engineering Conf., Honolulu, pp. 274-279, August 1997. |
4 | MIL-STD-1760E : Aircraft/store electrical interconnection system, U.S. DoD, 24 Oct. 2007. |
5 | MIL-STD-704F : Aircraft Electric Power Characteristics, U.S. Department of Defense, 12 March 2004. |
6 | Hee chae Woo, "Design and verification of electrical system for unmanned aerial vehicle through electrical load power analysis" Journal of the KIMST, Vol. 21, No.5, pp.675-683, Oct, 2018. |
7 | Hyeong seop Yeom, "A study on technique of development test by an aircraft captive flight test in weapon system" Journal of the Korean society for aeronautical & space sciences, Vol. 37, No.10, pp.1010-1016, Oct. 2009. DOI |
8 | Emadi, K.; Ehsani, M.; "Aircraft Power Systems: Technology, State of the Art, and Future Trends," Aerospace and Electronic Systems Magazine, IEEE Volume 15, Issue 1, pp. 28-32, Jan. 2000. DOI |
9 | Squair, M. J., "Safety, software architecture and MIL-STD-1760," in Proceedings of the 11th australian Workshop on Safety Critical Systems and Software, Adelaide: Australia, Vol. 29, pp.29~112, May 2007. |