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convert PrintSimulation listener to extension

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This commit is contained in:
JoePfeiffer 2022-12-07 15:22:28 -07:00
parent 17a4f1ffdb
commit f427cad09f
3 changed files with 66 additions and 34 deletions
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53
core/src/net/sf/openrocket/simulation/extension/example/PrintSimulation.java Normal file
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package net.sf.openrocket.simulation.extension.impl;
import net.sf.openrocket.simulation.FlightDataBranch;
import net.sf.openrocket.simulation.FlightDataType;
import net.sf.openrocket.simulation.FlightEvent;
import net.sf.openrocket.simulation.SimulationConditions;
import net.sf.openrocket.simulation.SimulationStatus;
import net.sf.openrocket.simulation.exception.SimulationException;
import net.sf.openrocket.simulation.extension.AbstractSimulationExtension;
import net.sf.openrocket.simulation.listeners.AbstractSimulationListener;
public class PrintSimulation extends AbstractSimulationExtension {
@Override
public void initialize(SimulationConditions conditions) throws SimulationException {
conditions.getSimulationListenerList().add(new PrintSimulationListener());
}
@Override
public String getName() {
return "Print Simulation Values";
}
@Override
public String getDescription() {
return "Print summary of simulation progress to standard output after every step";
}
private class PrintSimulationListener extends AbstractSimulationListener {
@Override
public boolean handleFlightEvent(SimulationStatus status, FlightEvent event) throws SimulationException {
System.out.println("*** handleEvent *** " + event.toString() +
" position=" + status.getRocketPosition() + " velocity=" + status.getRocketVelocity());
return true;
}
@Override
public void postStep(SimulationStatus status) throws SimulationException {
FlightDataBranch data = status.getFlightData();
System.out.printf("*** stepTaken *** time=%.3f position=" + status.getRocketPosition() +
" velocity=" + status.getRocketVelocity() + "=%.3f\n", status.getSimulationTime(), status.getRocketVelocity().length());
System.out.printf(" thrust=%.3fN drag==%.3fN mass=%.3fkg " +
"accZ=%.3fm/s2 acc=%.3fm/s2\n",
data.getLast(FlightDataType.TYPE_THRUST_FORCE),
data.getLast(FlightDataType.TYPE_DRAG_FORCE),
data.getLast(FlightDataType.TYPE_MASS),
data.getLast(FlightDataType.TYPE_ACCELERATION_Z),
data.getLast(FlightDataType.TYPE_ACCELERATION_TOTAL));
}
}
}

13
core/src/net/sf/openrocket/simulation/extension/example/PrintSimulationProvider.java Normal file
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package net.sf.openrocket.simulation.extension.impl;
import net.sf.openrocket.plugin.Plugin;
import net.sf.openrocket.simulation.extension.AbstractSimulationExtensionProvider;
@Plugin
public class PrintSimulationProvider extends AbstractSimulationExtensionProvider {
public PrintSimulationProvider() {
super(PrintSimulation.class, "Reports", "Print Simulation");
}
}

34
core/src/net/sf/openrocket/simulation/listeners/example/PrintSimulationListener.java
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@ -1,34 +0,0 @@
package net.sf.openrocket.simulation.listeners.example;
import net.sf.openrocket.simulation.FlightDataBranch;
import net.sf.openrocket.simulation.FlightDataType;
import net.sf.openrocket.simulation.FlightEvent;
import net.sf.openrocket.simulation.SimulationStatus;
import net.sf.openrocket.simulation.exception.SimulationException;
import net.sf.openrocket.simulation.listeners.AbstractSimulationListener;
public class PrintSimulationListener extends AbstractSimulationListener {
@Override
public boolean handleFlightEvent(SimulationStatus status, FlightEvent event) throws SimulationException {
System.out.println("*** handleEvent *** " + event.toString() +
" position=" + status.getRocketPosition() + " velocity=" + status.getRocketVelocity());
return true;
}
@Override
public void postStep(SimulationStatus status) throws SimulationException {
FlightDataBranch data = status.getFlightData();
System.out.printf("*** stepTaken *** time=%.3f position=" + status.getRocketPosition() +
" velocity=" + status.getRocketVelocity() + "=%.3f\n", status.getSimulationTime(), status.getRocketVelocity().length());
System.out.printf(" thrust=%.3fN drag==%.3fN mass=%.3fkg " +
"accZ=%.3fm/s2 acc=%.3fm/s2\n",
data.getLast(FlightDataType.TYPE_THRUST_FORCE),
data.getLast(FlightDataType.TYPE_DRAG_FORCE),
data.getLast(FlightDataType.TYPE_MASS),
data.getLast(FlightDataType.TYPE_ACCELERATION_Z),
data.getLast(FlightDataType.TYPE_ACCELERATION_TOTAL));
}
}