NASA NTRS · 19830007045
Advanced flight control system study
Abstract
The architecture, requirements, and system elements of an ultrareliable, advanced flight control system are described. The basic criteria are functional reliability of 10 to the minus 10 power/hour of flight and only 6 month scheduled maintenance. A distributed system architecture is described, including a multiplexed communication system, reliable bus controller, the use of skewed sensor arrays, and actuator interfaces. Test bed and flight evaluation program are proposed.
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Mcgough, J., Moses, K., Klafin, J. F.. 1982-11-01. Advanced flight control system study. https://ntrs.nasa.gov/citations/19830007045
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