Adaptive oscillatory fault monitoring

摘要

Systems, media, and methods are provided for oscillation monitoring. An aircraft system includes a first oscillation monitoring module and a second oscillation monitoring module. The first oscillation monitoring module is configured to select first oscillating portions of an input signal, generate a frequency signal that indicates a frequency of the first oscillating portions, and generate a first failure signal in response to the frequency of the first oscillating portions exceeding first oscillatory fault detection requirements for the input signal. The second oscillation monitoring module is configured to select second oscillating portions of the input signal based on the frequency signal generated by the first oscillation monitoring module and to generate a second failure signal in response to a frequency of the second oscillating portions exceeding second oscillatory fault detection requirements for the input signal.

主权项

1. An aircraft system comprising:
a third oscillation monitoring module configured to:
select third oscillating portions of an input signal;generate a frequency signal that indicates a frequency of the third oscillating portions; andgenerate a third failure signal in response to the frequency of the third oscillating portions exceeding third oscillatory fault detection requirements for the input signal; and a second oscillation monitoring module configured to:
select second oscillating portions of the input signal based on the frequency signal generated by the third oscillation monitoring module; andgenerate a second failure signal in response to a frequency of the second oscillating portions exceeding second oscillatory fault detection requirements for the input signal.