Edge filling method for monitoring data of plane airborne equipment
A technology for monitoring data and airborne equipment, applied to measuring devices, force/torque/power measuring instruments, instruments, etc., can solve the problem of not maintaining the edge characteristics of data well, and achieve the effect of maintaining edge characteristics and realizing reconstruction
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[0027] The present invention will be further described below in conjunction with the accompanying drawings and embodiments.
[0028] Step 1: y(i) is the brake pressure signal of the left inner wheel of a certain type of aircraft during a flight, where i=1,...N, and the corresponding spatial coordinates are x(i), where i=1,... N, assuming that the length of the processing window is L, that is, each signal segment contains L known signal sampling points, and for the missing sampling point to be recovered whose spatial coordinate is z, the nearest known sampling point behind it is the Ith, A total of L-1 signal segments contain the missing sampling point, and there is an adjacent signal segment before and after the missing sampling point. Among the L+1 signal segments, the signal data contained in the lth signal segment is :
[0029] [y(I-L+l-1),...,y(I+l-2)]l=1,....L+1. (1)
[0030] For the l-th signal segment, the data fitting of the signal segment is realized by an m-order p...
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