Protection Devices for Aircraft Electrical Power Distribution Systems: State of the Art
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Antonio Lázaro | Marina Sanz | Daniel Izquierdo | Andrés Barrado | C. Raga | A. Barrado | D. Izquierdo | A. Lázaro | M. Sanz | C. Raga
[1] Cary Spitzer. The All-Electric Aircraft: A Systems View and Proposed NASA Research Programs , 1984, IEEE Transactions on Aerospace and Electronic Systems.
[2] P. Zumel,et al. Protection devices for aircraft electrical power distribution systems: a survey , 2008, 2008 34th Annual Conference of IEEE Industrial Electronics.
[3] M. David Kankam,et al. A Survey of Power Electronics Applications in Aerospace Technologies , 2001 .
[4] Xiaohu Feng,et al. SiC based solid state power controller , 2008, 2008 Twenty-Third Annual IEEE Applied Power Electronics Conference and Exposition.
[5] Kenneth A. LaBel,et al. Implications of single event effect characterization of hybrid DC-DC converters and a solid state power controller , 1995 .
[6] D.L. Schweickart,et al. An evaluation of diagnostic techniques relevant to arcing fault current interrupters for direct current power systems in future aircraft , 2005, Proceedings Electrical Insulation Conference and Electrical Manufacturing Expo, 2005..
[7] A. Lazaro,et al. SSPC model with variable reset time, environmental temperature compensation and thermal memory effect , 2008, 2008 Twenty-Third Annual IEEE Applied Power Electronics Conference and Exposition.
[8] S. J. Cutts,et al. A collaborative approach to the More Electric Aircraft , 2002 .
[9] Kwa-Sur Tam,et al. Modeling the protection system components of the space station electric power system , 1994 .
[10] F. C. Lee,et al. Modeling and stability analysis of a DC power system with solid state power controllers , 1996, Proceedings of Applied Power Electronics Conference. APEC '96.
[11] S. Krstic,et al. 270-V Dc Hybrid Switch , 1986 .
[12] Dushan Boroyevich,et al. Subsystem Interaction Analysis in Power Distribution Systems of Next Generation Airlifters , 2002 .
[13] M. Howse,et al. All-electric aircraft , 2003 .
[14] A. J. Forsyth,et al. Distributed Electrical Power Management Architecture , 1999 .
[15] Boeing Phantom,et al. SUBSYSTEM DESIGN AND INTEGRATION FOR THE MORE ELECTRIC AIRCRAFT , 2007 .
[16] Mehrdad Ehsani,et al. Aircraft power systems: technology, state of the art, and future trends , 2000 .
[17] W. Liu,et al. A novel high current solid state power controller , 2005, 31st Annual Conference of IEEE Industrial Electronics Society, 2005. IECON 2005..
[18] Dominique Planson,et al. Silicon carbide power devices , 1998, 1998 International Semiconductor Conference. CAS'98 Proceedings (Cat. No.98TH8351).
[19] J. R. Todd,et al. Integrating fly-by-light systems , 1992, [1992] Proceedings IEEE/AIAA 11th Digital Avionics Systems Conference.
[20] J. J. Simon. State of the art in solid state power controller for aeronautical application , 2002 .
[21] J.A. Ortega,et al. Moving towards a more electric aircraft , 2007, IEEE Aerospace and Electronic Systems Magazine.
[22] P. Walia,et al. Power Management and Distribution System for a More-Electric Aircraft (MADMEL)-program status , 1997, IECEC-97 Proceedings of the Thirty-Second Intersociety Energy Conversion Engineering Conference (Cat. No.97CH6203).
[23] J. R. Todd. Direct optical control: a lightweight backup consideration , 1992, Proceedings of the IEEE 1992 National Aerospace and Electronics Conference@m_NAECON 1992.
[24] S. Yanabu,et al. A Solid-State Current Limiting Switch for Application of Large-scale Space Power Systems , 2007, 2007 IEEE Power Electronics Specialists Conference.
[25] Krishna Shenai,et al. Silicon carbide power converters for next generation aerospace electronics applications , 2000, Proceedings of the IEEE 2000 National Aerospace and Electronics Conference. NAECON 2000. Engineering Tomorrow (Cat. No.00CH37093).
[26] Göran Engdahl,et al. A new high power density generation system , 2006 .
[27] Sudip K. Mazumder,et al. Optically-triggered Power Transistor (OTPT) for Fly-by-light (FBL) and EMI-susceptible Power Electronics , 2006 .
[28] Dr. Cynthia Furse. Finding Fault : Locating Hidden Hazards on Aircraft Wiring , 2022 .
[29] M. K. Kazimierczuk,et al. High-temperature performance characterization of buck converter using SiC and Si devices , 1998, PESC 98 Record. 29th Annual IEEE Power Electronics Specialists Conference (Cat. No.98CH36196).
[30] David L. Daggett,et al. FUEL CELL DEMONSTRAT OR AIRPLANE , 2003 .
[31] S.N. Friedman. Solid-state power controller for the next generation , 1992, IEEE Aerospace and Electronic Systems Magazine.
[32] I. Cotton,et al. Higher voltage aircraft power systems , 2008, IEEE Aerospace and Electronic Systems Magazine.
[33] M.W. Stavnes,et al. Assessment of safety in space power wiring systems , 1994, IEEE Aerospace and Electronic Systems Magazine.
[34] John M. Maxwell,et al. A Configurable Solid State Power Management and Distribution System , 2002 .
[35] M. Mohadjer,et al. A Solid State Power Controller Module for the International Space Station EXPRESS Rack , 1997, IECEC-97 Proceedings of the Thirty-Second Intersociety Energy Conversion Engineering Conference (Cat. No.97CH6203).