Requirements and specifications for a method of optimizing the design of fault-tolerant flight control systems are provided. Algorithms that could be used for developing new and modifying existing computer programs are also provided, with recommendations for follow-on work.
Cost and Benefits Design Optimization Model for Fault Tolerant Flight Control Systems
1982
251 pages
Report
No indication
English
Synchronous fault-tolerant flight control systems
AIAA | 1981
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