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| author | Nao Pross <np@0hm.ch> | 2024-05-31 15:31:02 +0200 |
|---|---|---|
| committer | Nao Pross <np@0hm.ch> | 2024-05-31 15:31:02 +0200 |
| commit | d2d174694099a2e9e88124287e2fd32c3cc4e808 (patch) | |
| tree | 5bb4a53a820ec32d175845a9062888fdb26b4f96 /uav_sim_step.m | |
| parent | Add worst case (diff) | |
| download | uav-d2d174694099a2e9e88124287e2fd32c3cc4e808.tar.gz uav-d2d174694099a2e9e88124287e2fd32c3cc4e808.zip | |
Diffstat (limited to 'uav_sim_step.m')
| -rw-r--r-- | uav_sim_step.m | 17 |
1 files changed, 11 insertions, 6 deletions
diff --git a/uav_sim_step.m b/uav_sim_step.m index 7bf0f2b..d7facbf 100644 --- a/uav_sim_step.m +++ b/uav_sim_step.m @@ -146,11 +146,16 @@ if do_plots to_deg = 180 / pi; % radians to degrees to_rpm = pi / 30; % rad / s to RPM + delta = ''; + if isfield(uncert, 'Delta') + delta = 'with $\Delta$'; + end + % Figure for flaps and Euler angles figure; sgtitle(sprintf(... - '\\bfseries Step Response of Flap and Euler Angles (%s)', ... - ctrl.Name), 'Interpreter', 'latex'); + '\\bfseries Step Response of Flap and Euler Angles (%s) %s', ... + ctrl.Name, delta), 'Interpreter', 'latex'); % Plot limits alpha_max_deg = params.actuators.ServoAbsMaxAngle * to_deg; @@ -256,8 +261,8 @@ if do_plots % Plot step response from z to omega figure; sgtitle(sprintf(... - '\\bfseries Step Response to Propeller (%s)', ... - ctrl.Name), 'Interpreter', 'latex'); + '\\bfseries Step Response to Propeller (%s) %s', ... + ctrl.Name, delta), 'Interpreter', 'latex'); hold on; step(P_clp(idx.PlotOmega, idx.InputReference(3)) * to_rpm, T); @@ -273,8 +278,8 @@ if do_plots % Figure for position and velocity figure; sgtitle(sprintf(... - '\\bfseries Step Response of Position and Speed (%s)', ... - ctrl.Name), 'Interpreter', 'latex'); + '\\bfseries Step Response of Position and Speed (%s) %s', ... + ctrl.Name, delta), 'Interpreter', 'latex'); % Plot step response from horizontal reference to horizontal position subplot(2, 2, 1); hold on; |