Figure 7.9. File AERO.c: I/O
data set
This model structure is also compatible with the complexity estimation provided by the functions estorderiv.m (MATLAB®) or estorderiv.sci (Scilab) (estimation with the method of instrumental variable with delayed inputs) that gives n = max (nA,nB+d) = 2 and nA=1, nB=2, d=0 respectively (see Figure 7.10).
Another identification is thus carried
out with the same structure,
method and adaptation gain, but with
nB=2, d=0, nA=1.
The results obtained are as follows:
S = 1 M = 1 (RLS)
A = 1 FILE:AERO.C NS = 128 DELAY D=0 COEFFICIENTS OF POLYNOMIAL A: A(1) = -0.6672 COEFFICIENTS OF POLYNOMIAL B: B(1) = 0.1736
B(2) = 0.0545
VALIDATION TEST: Whiteness of the residual error
System variance: 0.0035 Model variance: 0.0034 Error variance R(0): 3.991 E-04