Digital Flight Control System EMI/EMP Testing-Lessons Learned

831411

10/03/1983

Authors Abstract
Content
A laboratory test facility has been developed to apply full-scale lightning and EMP fields to safety-critical digital flight control systems early in the development process. Such testing enables relatively low-cost evaluation of system susceptibility, allows in-depth study of the effects of disturbances, and provides essential feedback to system engineers attempting to harden the design. Results indicate that:
  • Proper design practice results in systems that can tolerate fields associated with lightning strikes or EMP to levels projected within a metal-skinned aircraft.
  • Lightning/EMP tests do uncover design faults and are of value early in the development process.
  • Optical data bus mechanization outperformed a conventional wire bus in high-level transient fields, as expected.
Meta TagsDetails
DOI
https://doi.org/10.4271/831411
Pages
9
Citation
Bailey, D., and Graves, G., "Digital Flight Control System EMI/EMP Testing-Lessons Learned," SAE Technical Paper 831411, 1983, https://doi.org/10.4271/831411.
Additional Details
Publisher
Published
Oct 3, 1983
Product Code
831411
Content Type
Technical Paper
Language
English