McConnell, R. (1988). Avionics System Design for High Energy Fields (Report No. DOT/FAA/CT-87/19). United States. Department of Transportation. Federal Aviation Administration. William J. Hughes Technical Center. https://rosap.ntl.bts.gov/view/dot/92920
McConnell, R.. Avionics System Design for High Energy Fields. Report no. DOT/FAA/CT-87/19. United States. Department of Transportation. Federal Aviation Administration. William J. Hughes Technical Center, 1988. https://rosap.ntl.bts.gov/view/dot/92920.
McConnell, R. Avionics System Design for High Energy Fields. United States. Department of Transportation. Federal Aviation Administration. William J. Hughes Technical Center, 1988, Report no. DOT/FAA/CT-87/19, ROSA P. https://rosap.ntl.bts.gov/view/dot/92920.
Because of the significant differences in transient susceptibility, the use of digital electronics in flight critical systems, and the reduced shielding effects of composite materials, there is a definite need to define design practices which will minimize electromagnetic susceptibility, to investigate the operational environment, and to develop appropriate testing methods or flight critical systems.
McConnell, R. (1988). Avionics System Design for High Energy Fields (Report No. DOT/FAA/CT-87/19). United States. Department of Transportation. Federal Aviation Administration. William J. Hughes Technical Center. https://rosap.ntl.bts.gov/view/dot/92920
McConnell, R.. Avionics System Design for High Energy Fields. Report no. DOT/FAA/CT-87/19. United States. Department of Transportation. Federal Aviation Administration. William J. Hughes Technical Center, 1988. https://rosap.ntl.bts.gov/view/dot/92920.
McConnell, R. Avionics System Design for High Energy Fields. United States. Department of Transportation. Federal Aviation Administration. William J. Hughes Technical Center, 1988, Report no. DOT/FAA/CT-87/19, ROSA P. https://rosap.ntl.bts.gov/view/dot/92920.
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