1. Aircraft Internal Time Division Command/Response Multiple Data Bus, Military Standard MIL-STD-1553B, September 1978.
2. Computer: An Investigation of the Theory and Practice of Fault-Tolerant Computer Design, IEEE Transactions on Computers, Vol. C-20, No. 11, November 1971, pp. 1312–1321.
3. Avizienis, A., The Four-Universe Information System Model for the Study of Fault Tolerance, Proceedings of the 12th Annual International Symposium on Fault-Tolerant Computing, Santa Monica, California, June 22-24, 1982, pp. 6–13.
4. Ayache, J., J. Courtiat, and M. Diaz, REBUS: A Fault Tolerant Distributed System for Industrial Real-Time Control, IEEE Transactions on Computers, Vol. C-31, No. 7, July 1982, pp. 637–647.
5. Bosch, J. A. and W. J. Kuehl,4 Reconfigurable Redundancy Management for Aircraft Flight Control, Journal of Aircraft, Vol. 14, No. 10, October 1977, pp. 966–971.