Migration to OpenModelica 1.25 and FMUs Generation

SimulationModels/OpenModelica 1.11/AIDAModelica/ComputeTotalThrustCA.mo

@@ -0,0 +1,57 @@
+// CP: 65001
+// SimulationX Version: 3.8.2.45319 x64
+within AIDAModelica;
+model ComputeTotalThrustCA "[SF2.4.2] Compute total thrust"
+	Modelica.Blocks.Interfaces.RealInput AccelerationConsign(
+		quantity="Mechanics.Translation.Accel",
+		displayUnit="m/s²") "Acceleration consign" annotation(Placement(
+		transformation(extent={{-20,-20},{20,20}}),
+		iconTransformation(extent={{-120,-20},{-80,20}})));
+	Modelica.Blocks.Interfaces.RealOutput TotalThrustAP(
+		quantity="Mechanics.Translation.Force",
+		displayUnit="N") "Total thrust autopilot mode" annotation(Placement(
+		transformation(extent={{-10,-10},{10,10}}),
+		iconTransformation(extent={{90,-10},{110,10}})));
+	parameter Real m(
+		quantity="Basics.Mass",
+		displayUnit="kg")=1.8 "Parameter m";
+	Real AC(
+		quantity="Mechanics.Translation.Velocity",
+		displayUnit="m/s") "Altitude consign";
+	parameter Real N=-1 "Acceleration linear threshold";
+	equation
+		// enter your equations here
+		AC = AccelerationConsign;
+		
+		//TotalThrustAP =if AC<0 then -m*AC else 0;
+		//to prevent loss of attitude control due to a nul thrust
+		TotalThrustAP =if AC<N then -m*AC else -m*N*exp(1/N*(AC-N));
+	annotation(
+		Icon(graphics={
+			Rectangle(
+				fillColor={255,255,255},
+				fillPattern=FillPattern.Solid,
+				extent={{-100,100},{100,-100}}),
+			Text(
+				textString="* m",
+				fillPattern=FillPattern.None,
+				extent={{-70,26.7},{73.3,-30}}),
+			Line(
+				points={{-3.3,76.7},{-3.3,76.7},{0,-76.7}},
+				color={192,192,192},
+				arrow={Arrow.Filled,Arrow.None}),
+			Line(
+				points={{-1.1,51.1},{-1.1,51.1},{8.4,-104.1}},
+				color={192,192,192},
+				arrow={Arrow.Filled,Arrow.None},
+				origin={24.4,-63.7},
+				rotation=-93),
+			Line(
+				points={{-81.09999999999999,95.59999999999999},{8.9,-47.8},{72.2,-47.8}},
+				origin={-8.9,-18.9})}),
+		experiment(
+			StopTime=1,
+			StartTime=0,
+			Interval=0.002,
+			MaxInterval="0.001"));
+end ComputeTotalThrustCA;