Performance analysis of high-speed MIL-STD-1553 bus system using DMT technology

With the rapid development of modern avionics system, traditional MIL-STD-1553 bus cannot meet the requirements of high-speed communication. In this paper, a method of improving the transmission rate of the avionics bus is purposed by implementing a Discrete Multitone (DMT) interface over existing MIL-STD-1553 bus. Physical layer and analog front end (AFE) are designed and analyzed in detail. This solution has been evaluated on FPGA platform and is demonstrated to be effective. The maximum data rate can achieve 100Mbit/s. It shows a tremendous performance improvement, as well as significant cost savings by keeping using legacy devices and MILSTD-1553 cables.

[1]  I. Djokovic Cyclic prefix extension in DMT systems , 1998, Conference Record of Thirty-Second Asilomar Conference on Signals, Systems and Computers (Cat. No.98CH36284).

[2]  Jianjun Lei,et al.  A novel method for evaluating the attenuation of 1553B bus system , 2012, 2012 7th International Conference on Computer Science & Education (ICCSE).

[3]  Cui Chao,et al.  Implementation and analysis of broadband OFDM high-rate data interface to aviation bus , 2008, 2008 11th IEEE International Conference on Communication Technology.

[4]  H. Hartmann Spectrum of Manchester Coded FSK , 1972, IEEE Trans. Commun..

[5]  M.G. Hegarty High performance 1553: a feasibility study , 2004, The 23rd Digital Avionics Systems Conference (IEEE Cat. No.04CH37576).

[6]  Russ Duren Options For Upgrading Legacy Avionics Systems , 2006, J. Aerosp. Comput. Inf. Commun..