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-rw-r--r--uav_uncertainty.m26
1 files changed, 24 insertions, 2 deletions
diff --git a/uav_uncertainty.m b/uav_uncertainty.m
index aff30ca..b664cee 100644
--- a/uav_uncertainty.m
+++ b/uav_uncertainty.m
@@ -37,9 +37,11 @@ eps_alpha = max(eps_l + eps_S + 2 * eps_omega, eps_S + eps_d + eps_omega);
% W_momega = eps_omega * 10 / (s + 10);
% W_mState = .01 * 10 / (s + 10);
-W_malpha = eps_alpha * tf(1);
+b = 1e3;
+
+W_malpha = make_weight(b, 1 / eps_alpha, 1e-2);
W_momega = tf(0);
-W_mState = .01 * tf(1);
+W_mState = 1 - 1 / (s / 50 + 1);
uncert = struct(...
'FlapAngle', W_malpha * eye(4), ...
@@ -61,4 +63,24 @@ if do_plots
end
end
+
+% Make a n-order performance weight function
+%
+% Arguments:
+% OMEGA Cutting frequency (-3dB)
+% A Magnitude at DC, i.e. |Wp(0)|
+% M Magnitude at infinity, i.e. |Wp(inf)|
+% ORD Order
+function [Wp] = make_weight(omega, A, M, ord)
+
+if nargin > 3
+ n = ord;
+else
+ n = 1;
+end
+
+s = tf('s');
+Wp = (s / (M^(1/n)) + omega)^n / (s + omega * A^(1/n))^n;
+
+end
% vim: ts=2 sw=2 et: