This research involves the development of a knowledge-based fault-tolerant flight control system. A software architecture is presented that integrates quantitative analytical redundancy techniques and heuristic expert system problem solving concepts for the purpose of in-flight, real-time failure accommodation.
Fault-tolerant flight control system combining expert system and analytical redundancy concepts
1987-07-01
Conference paper
No indication
English
Fault tolerant digital flight control using analytical redundancy
Tema Archive | 1977
|Dual-redundancy steer-by-wire redundancy fault-tolerant control system
European Patent Office | 2025
|