Migration to OpenModelica 1.25 and FMUs Generation

2026-05-26 09:37:35 +02:00
parent fdf293ece6
commit fe90b840ed
370 changed files with 968105 additions and 743 deletions
--- a/1.11/AIDAModelica/ControlAltitude.mo
+++ b/1.11/AIDAModelica/ControlAltitude.mo
@@ -0,0 +1,92 @@
+// CP: 65001
+// SimulationX Version: 3.8.2.45319 x64
+within AIDAModelica;
+model ControlAltitude "[SF2.4] Control altitude"
+	Modelica.Blocks.Interfaces.RealOutput TotalThrustManual(
+		quantity="Mechanics.Translation.Force",
+		displayUnit="N") "Desired total thrust autopilot mode output" annotation(Placement(
+		transformation(extent={{20,20},{40,40}}),
+		iconTransformation(
+			origin={100,0},
+			extent={{-10,-10},{10,10}})));
+	Modelica.Blocks.Interfaces.RealInput VSpeed(
+		quantity="Mechanics.Translation.Velocity",
+		displayUnit="m/s") "Real drone speed feedback" annotation(Placement(
+		transformation(extent={{-105,-5},{-65,35}}),
+		iconTransformation(extent={{-120,30},{-80,70}})));
+	Modelica.Blocks.Interfaces.RealInput RCVerticalSpeedCommand(
+		quantity="Mechanics.Translation.Velocity",
+		displayUnit="m/s") "'input Real' as connector" annotation(Placement(
+		transformation(extent={{-105,25},{-65,65}}),
+		iconTransformation(
+			origin={-100,-50},
+			extent={{-20,-20},{20,20}})));
+	ComputeTotalThrustCA computeTotalThrustCA1 annotation(Placement(transformation(extent={{-10,20},{10,40}})));
+	ComputeAltitudeConsign computeAltitudeConsign1 annotation(Placement(transformation(extent={{-55,20},{-35,40}})));
+	equation
+		connect(computeAltitudeConsign1.VSpeed,VSpeed) annotation(Line(
+			points={{-54,26},{-76,26},{-76,16},{-84,16}},
+			color={0,0,127}));
+				connect(computeTotalThrustCA1.AccelerationConsign,computeAltitudeConsign1.AccelerationConsign) annotation(Line(
+			points={{-10,30},{-15,30},{-30,30},{-35,30}},
+			color={0,0,127},
+			thickness=0.0625));
+				connect(computeAltitudeConsign1.RCVerticalSpeedCommand,RCVerticalSpeedCommand) annotation(Line(
+			points={{-55,35},{-60,35},{-80,35},{-80,45},{-85,45}},
+			color={0,0,127},
+			thickness=0.0625));
+				
+		connect(computeTotalThrustCA1.TotalThrustAP,TotalThrustManual) annotation(Line(
+			points={{10,30},{15,30},{25,30},{30,30}},
+			color={0,0,127},
+			thickness=0.0625));
+	annotation(
+		Speed(flags=2),
+		TotalThrustManual(flags=2),
+		RCVerticalSpeedCommand(flags=2),
+		computeTotalThrustCA1(
+			AccelerationConsign(flags=2),
+			TotalThrustAP(flags=2),
+			AC(flags=2)),
+		computeAltitudeConsign1(
+			RCVerticalSpeedCommand(flags=2),
+			AccelerationConsign(flags=2),
+			PID1(
+				u(flags=2),
+				y(flags=2),
+				P(
+					u(flags=2),
+					y(flags=2)),
+				I(
+					u(flags=2),
+					y(flags=2)),
+				D(
+					u(flags=2),
+					y(flags=2),
+					x(flags=2)),
+				Gain(
+					u(flags=2),
+					y(flags=2)),
+				Add(
+					u1(flags=2),
+					u2(flags=2),
+					u3(flags=2),
+					y(flags=2))),
+			speedErrorModelSAC1(
+				SpeedConsign(flags=2),
+				Speed(flags=2),
+				SpeedError(flags=2),
+				vzd(flags=2),
+				vz(flags=2),
+				ASE(flags=2))),
+		Icon(graphics={
+			Rectangle(
+				fillColor={255,255,255},
+				fillPattern=FillPattern.Solid,
+				extent={{-100,100},{100,-100}})}),
+		experiment(
+			StopTime=1,
+			StartTime=0,
+			Interval=0.002,
+			MaxInterval="0.001"));
+end ControlAltitude;