Method of displaying data in an aircraft
A method and apparatus of displaying data in an aircraft, the method including receiving data, from at least one sensor operably coupled to the aircraft, averaging, by a control module, at least two data points of the received data to define a delta and averaged data, comparing, by the control module, the delta to a reference threshold value, and providing an indication, on a display of the aircraft, of the averaged data based on the comparing.
1. A method of displaying data in an aircraft, the method comprising:
receiving data, from at least one sensor operably coupled to the aircraft, relevant to vibration of the aircraft during flight to define received data;
averaging, by a control module, at least two data points of the received data to define a delta and averaged vibration data;
comparing, by the control module, the delta to a reference threshold value;
providing an indication, on a display of the aircraft, of the averaged vibration data based on the comparing; and
repeating the receiving data, averaging, comparing, and providing an indication and where when the delta is above the reference threshold value the averaged vibration data is based on two data points and when the delta is below the reference threshold value subsequent averaging includes more than two data points.
2. The method of claim 1 wherein the repeating comprises continuously repeating.
3. The method of claim 2 wherein the continuously repeating comprises continuously repeating at set time intervals.
4. The method of claim 1 , further comprising increasing the number of data points used in a subsequent averaging when the delta is below the reference threshold value.
5. The method of claim 4 , further comprising capping the number of data points used in the subsequent averaging at a capped threshold.
6. The method of claim 5 , further comprising counting a number of data points used in the averaging and incrementing by one on each subsequent averaging until the capped threshold is reached.
7. The method of claim 1 , wherein the at least two data points are a current value and a most recent value.
8. The method of claim 1 , wherein the reference threshold value is greater than 38.1 micrometers peak displacement.
9. The method of claim 1 , wherein the received data is from at least one accelerometer.
10. A method of displaying data in an aircraft, the method comprising:
receiving data, from at least one sensor operably coupled to the aircraft, relevant to vibration of the aircraft during flight to define received data;
determining, by a control module, a difference between at least two data points of the received data to define a delta;
comparing, by the control module, the delta to a reference threshold value;
averaging, by the control module, a predetermined number of data points based on the comparing to define averaged vibration data, wherein the predetermined number of data points is incremented when the delta is below the reference threshold value; and
providing an indication, on a display of the aircraft, of the averaged vibration data.
11. The method of claim 10 , wherein the at least two data points are a current value and a most recent value.
12. The method of claim 10 , wherein the reference threshold value is greater than 38.1 micrometers peak displacement.
13. The method of claim 10 , wherein the predetermined number of data points is two when the delta is above the reference threshold value.
14. The method of claim 10 wherein the predetermined number of data points is one of a range of a predetermined number of data points.
15. The method of claim 14 , further comprising determining the one of a range of predetermined number of points.
16. A method of displaying data in an aircraft, the method comprising:
a) receiving data, from at least one sensor operably coupled to the aircraft, relevant to vibration of the aircraft during flight to define received data;
b) determining, by a control module, a difference between at least two data points of the received data to define a delta;
c) comparing, by the control module, the delta to a reference delta threshold value;
d) averaging, by the control module, a predetermined number of data points based on the comparing to define averaged vibration data, wherein the predetermined number of data points is incremented when the delta is below the reference delta threshold value;
e) providing a decimal value, on a display of the aircraft, of the averaged vibration data; and
f) repeating a)-e) to provide a rolling averaged vibration data.
17. The method of claim 16 , further comprising determining when the averaged vibration data is above a predetermined threshold.
18. The method of claim 17 , further comprising providing an alert to indicate the determined vibration.
19. The method of claim 16 , further comprising counting a number of data points used in the averaging and incrementing by one on each subsequent averaging until a threshold is reached.