NASA NTRS · 20120010616
Tunable architecture for aircraft fault detection
Abstract
A method for detecting faults in an aircraft is disclosed. The method involves predicting at least one state of the aircraft and tuning at least one threshold value to tightly upper bound the size of a mismatch between the at least one predicted state and a corresponding actual state of the non-faulted aircraft. If the mismatch between the at least one predicted state and the corresponding actual state is greater than or equal to the at least one threshold value, the method indicates that at least one fault has been detected.
Keep this discovery
Explore connections, maps & timelines
Ganguli, Subhabrata, Papageorgiou, George, Glavaski-Radovanovic, Sonja. 2012-06-26. Tunable architecture for aircraft fault detection. https://ntrs.nasa.gov/citations/20120010616
Cite the original work for its findings. Save a collection to share your selection of sources.