Autors: Todorov, G. D., Kamberov, K. H., Zlatev, B. N.
Title: Approach for Assessment of Electronics Control Unit for Airborne Application Through Virtual Prototyping
Keywords: Electronic box, fatigue, Power Spectral Density, PSD, vibration

Abstract: In this paper an electronic box for VTOL airborne application is analysed based on its' structural integrity through different vibration spectres based on the Power Spectral Density analysis. Using this methodology, the life expectancy of the electronic box is calculated based on FEM analysis before the physical tests are performed for validation at a following stage.

References

  1. P. Stoica and R. Moses, Spectral Analysis of Signals, New Jersey: Prentice Hall, Inc., 2005.
  2. W. Bialek, R. d. R. van Steveninck, F. Rieke and D. Warland, pikes: Exploring the Neural Code (Computational Neuroscience), MIT Press, 1996.
  3. S. Millers and D. Childers, Probability and random processes., Academic Press; 2nd edition, 2012.
  4. J. Y. Stein, Digital Signal Processing: A Computer Science Perspective, John Wiley & Sons, Inc, 2000.
  5. A. Birolini, Reliability Engineering: Theory and Practice, Berlin: Springer-Verlag Berlin Heidelberg, 2007.
  6. S. Babaeizadeh, S. H. Zhou, X. Liu, W. Y. Hu, D. Q. Feild, E. D. Helfenbein, R. E. Gregg and J. M. Lindauer, "A novel heart rate variability index for evaluation of left ventricular function using five-minute electrocardiogram, " in Computers in Cardiology, Newcastle upon Tyne, 2007.
  7. Radio Technical Commission for Aeronautics, Inc., DO-160, 2010.
  8. Y.-L. Lee, M. E. Barkey and H.-T. Kang, Metal Fatigue Analysis Handbook, Elsevier, Inc., 2012.

Issue

2024 59th International Scientific Conference on Information, Communication and Energy Systems and Technologies, ICEST 2024 - Proceedings, 2024, , https://doi.org/10.1109/ICEST62335.2024.10639799

Вид: публикация в международен форум, публикация в реферирано издание, индексирана в Scopus