Systems and methods for diagnosing aircraft failure are provided. In one embodiment, a method can include receiving a first set of data from an aircraft in flight indicative of a failure event associated with the aircraft. The first set of data can be indicative of at least one or more conditions associated with the aircraft. The method can include performing one or more computer-based simulations to generate one or more simulated failure events, based at least in part on the conditions. The method can include identifying one or more simulated causes associated with the simulated failure events. The method can include determining one or more potential causes of at least a portion of the failure event, based at least in part on the simulated causes. The method can include communicating a second set of data indicative of at least the potential causes, to the aircraft while it is in flight.
Real-time non-onboard diagnostics of aircraft failures
2017-03-29
Patent
Electronic Resource
English
Real time detection filters for the onboard diagnostics of incipient failures
Automotive engineering | 1989
|Real time detection filters for onboard diagnosis of incipient failures
Automotive engineering | 1989
|Real Time Detection Filters for Onboard Diagnosis of Incipient Failures
SAE Technical Papers | 1989
|