1 package net.sf.openrocket.optimization.rocketoptimization.parameters;
3 import net.sf.openrocket.document.Simulation;
4 import net.sf.openrocket.l10n.Translator;
5 import net.sf.openrocket.logging.LogHelper;
6 import net.sf.openrocket.optimization.general.OptimizationException;
7 import net.sf.openrocket.optimization.rocketoptimization.OptimizableParameter;
8 import net.sf.openrocket.simulation.FlightDataType;
9 import net.sf.openrocket.simulation.exception.MotorIgnitionException;
10 import net.sf.openrocket.simulation.exception.SimulationException;
11 import net.sf.openrocket.simulation.exception.SimulationLaunchException;
12 import net.sf.openrocket.simulation.listeners.system.ApogeeEndListener;
13 import net.sf.openrocket.startup.Application;
14 import net.sf.openrocket.unit.UnitGroup;
17 * An optimization parameter that computes the maximum acceleration during a simulated flight.
19 * @author Sampo Niskanen <sampo.niskanen@iki.fi>
21 public class MaximumAccelerationParameter implements OptimizableParameter {
23 private static final LogHelper log = Application.getLogger();
24 private static final Translator trans = Application.getTranslator();
27 public String getName() {
28 return trans.get("name");
32 public double computeValue(Simulation simulation) throws OptimizationException {
34 log.debug("Running simulation to evaluate maximum acceleration");
35 simulation.simulate(new ApogeeEndListener());
36 double value = simulation.getSimulatedData().getBranch(0).getMaximum(FlightDataType.TYPE_ACCELERATION_TOTAL);
37 log.debug("Maximum acceleration was " + value);
39 } catch (MotorIgnitionException e) {
40 // A problem with motor ignition will cause optimization to fail
41 throw new OptimizationException(e);
42 } catch (SimulationLaunchException e) {
43 // Other launch exceptions result in zero velocity
45 } catch (SimulationException e) {
46 // Other exceptions fail
47 throw new OptimizationException(e);
52 public UnitGroup getUnitGroup() {
53 return UnitGroup.UNITS_ACCELERATION;