Merge pull request #577 from wolsen/issue-576
Fix ground hit velocity calculation
This commit is contained in:
Daniel Williams
GitHub
commit
59a01b3877
@ -101,7 +101,7 @@ public class FlightData {
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for (FlightDataBranch b : branches)
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this.addBranch(b);
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calculateIntrestingValues();
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calculateInterestingValues();
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}
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@ -126,7 +126,7 @@ public class FlightData {
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branches.add(branch);
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if (branches.size() == 1) {
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calculateIntrestingValues();
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calculateInterestingValues();
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}
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}
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@ -185,7 +185,7 @@ public class FlightData {
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* Calculate the max. altitude/velocity/acceleration, time to apogee, flight time
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* and ground hit velocity.
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*/
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private void calculateIntrestingValues() {
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private void calculateInterestingValues() {
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if (branches.isEmpty())
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return;
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@ -195,13 +195,7 @@ public class FlightData {
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maxMachNumber = branch.getMaximum(FlightDataType.TYPE_MACH_NUMBER);
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flightTime = branch.getLast(FlightDataType.TYPE_TIME);
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if (branch.getLast(FlightDataType.TYPE_ALTITUDE) < 10) {
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groundHitVelocity = branch.getLast(FlightDataType.TYPE_VELOCITY_TOTAL);
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} else {
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groundHitVelocity = Double.NaN;
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}
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// Time to apogee
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List<Double> time = branch.get(FlightDataType.TYPE_TIME);
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List<Double> altitude = branch.get(FlightDataType.TYPE_ALTITUDE);
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@ -236,6 +230,10 @@ public class FlightData {
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double t = event.getTime();
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List<Double> velocity = branch.get(FlightDataType.TYPE_VELOCITY_TOTAL);
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deploymentVelocity = MathUtil.interpolate( time, velocity, t);
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} else if (event.getType() == FlightEvent.Type.GROUND_HIT) {
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double t = event.getTime();
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List<Double> velocity = branch.get(FlightDataType.TYPE_VELOCITY_TOTAL);
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groundHitVelocity = MathUtil.interpolate( time, velocity, t);
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}
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}
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285
core/test/net/sf/openrocket/simulation/TestFlightData.java
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285
core/test/net/sf/openrocket/simulation/TestFlightData.java
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@ -0,0 +1,285 @@
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package net.sf.openrocket.simulation;
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import static org.junit.Assert.assertEquals;
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import static org.junit.Assert.assertNotNull;
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import static org.junit.Assert.assertTrue;
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import org.junit.Test;
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import net.sf.openrocket.aerodynamics.WarningSet;
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/**
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* Tests the FlightData object.
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*
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* @author Billy Olsen
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*/
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public class TestFlightData {
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/**
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* Test method for {@link net.sf.openrocket.simulation.FlightData#FlightData()}.
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*/
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@Test
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public void testFlightData() {
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FlightData data = new FlightData();
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WarningSet warnings = data.getWarningSet();
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assertNotNull(warnings);
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assertTrue(warnings.isEmpty());
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assertEquals(0, data.getBranchCount());
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assertEquals(Double.NaN, data.getDeploymentVelocity(), 0.00);
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assertEquals(Double.NaN, data.getFlightTime(), 0.00);
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assertEquals(Double.NaN, data.getGroundHitVelocity(), 0.00);
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assertEquals(Double.NaN, data.getLaunchRodVelocity(), 0.00);
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assertEquals(Double.NaN, data.getMaxAcceleration(), 0.00);
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assertEquals(Double.NaN, data.getMaxAltitude(), 0.00);
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assertEquals(Double.NaN, data.getMaxMachNumber(), 0.00);
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assertEquals(Double.NaN, data.getTimeToApogee(), 0.00);
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}
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/**
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* Tests flight data created from summary data.
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*/
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@Test
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public void testFlightDataFromSummaryData() {
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double deploymentVelocity = 14.8;
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double flightTime = 69.1;
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double groundHitVelocity = 3.4;
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double launchRodVelocity = 17.5;
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double maxAcceleration = 156.2;
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double maxVelocity = 105.9;
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double maxAltitude = 355.1;
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double maxMachNumber = 0.31;
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double timeToApogee = 7.96;
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FlightData data = new FlightData(maxAltitude, maxVelocity, maxAcceleration,
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maxMachNumber, timeToApogee, flightTime,
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groundHitVelocity, launchRodVelocity,
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deploymentVelocity);
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WarningSet warnings = data.getWarningSet();
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assertNotNull(warnings);
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assertTrue(warnings.isEmpty());
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assertEquals(0, data.getBranchCount());
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assertEquals(deploymentVelocity, data.getDeploymentVelocity(), 0.00);
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assertEquals(flightTime, data.getFlightTime(), 0.00);
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assertEquals(groundHitVelocity, data.getGroundHitVelocity(), 0.00);
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assertEquals(launchRodVelocity, data.getLaunchRodVelocity(), 0.00);
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assertEquals(maxAcceleration, data.getMaxAcceleration(), 0.00);
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assertEquals(maxAltitude, data.getMaxAltitude(), 0.00);
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assertEquals(maxMachNumber, data.getMaxMachNumber(), 0.00);
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assertEquals(timeToApogee, data.getTimeToApogee(), 0.00);
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}
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/**
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* Test method for {@link net.sf.openrocket.simulation.FlightData#FlightData(net.sf.openrocket.simulation.FlightDataBranch[])}.
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*/
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@Test
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public void testFlightDataFlightDataBranchArray() {
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FlightData data = new FlightData(new FlightDataBranch("Test", FlightDataType.TYPE_TIME));
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WarningSet warnings = data.getWarningSet();
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assertNotNull(warnings);
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assertTrue(warnings.isEmpty());
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assertEquals(1, data.getBranchCount());
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data = new FlightData(new FlightDataBranch("Test 1", FlightDataType.TYPE_TIME),
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new FlightDataBranch("Test 2", FlightDataType.TYPE_TIME));
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warnings = data.getWarningSet();
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assertNotNull(warnings);
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assertTrue(warnings.isEmpty());
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assertEquals(2, data.getBranchCount());
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}
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private FlightDataBranch createFlightDataBranch(final String name, final FlightDataType dataType, final double[] values) {
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final FlightDataBranch branch = new FlightDataBranch(name, dataType);
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addDataPoints(branch, dataType, values);
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return branch;
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}
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private void addDataPoints(final FlightDataBranch branch, final FlightDataType dataType, final double[] values) {
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for (int i=0; i < values.length; i++) {
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branch.addPoint();
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branch.setValue(dataType, values[i]);
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}
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}
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/**
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* Test method for {@link net.sf.openrocket.simulation.FlightData#getMaxAltitude()}.
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*/
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@Test
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public void testGetMaxAltitudeCalculated() {
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final double[] altitudes = new double[] {
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10.5,
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37.771,
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37.5,
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5.1,
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0.0
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};
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FlightDataBranch branch =
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createFlightDataBranch("Test Max Alt", FlightDataType.TYPE_ALTITUDE, altitudes);
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FlightData data = new FlightData(branch);
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assertEquals(37.771, data.getMaxAltitude(), 0.000);
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}
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/**
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* Test method for {@link net.sf.openrocket.simulation.FlightData#getMaxVelocity()}.
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*/
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@Test
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public void testGetMaxVelocityCalculated() {
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final double[] velocities = new double[] {
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10.5,
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23.7,
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35.5,
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30.1,
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0.0
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};
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FlightDataBranch branch =
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createFlightDataBranch("Test Max Velocity", FlightDataType.TYPE_VELOCITY_TOTAL, velocities);
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FlightData data = new FlightData(branch);
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assertEquals(35.5, data.getMaxVelocity(), 0.000);
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}
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/**
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* Test method for {@link net.sf.openrocket.simulation.FlightData#getMaxMachNumber()}.
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*/
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@Test
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public void testGetMaxMachNumberCalculated() {
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final double[] machs = new double[] {
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0.1,
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0.2,
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0.333,
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0.3,
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0.1
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};
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FlightDataBranch branch =
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createFlightDataBranch("Test Max Mach", FlightDataType.TYPE_MACH_NUMBER, machs);
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FlightData data = new FlightData(branch);
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assertEquals(0.333, data.getMaxMachNumber(), 0.000);
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}
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/**
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* Test method for {@link net.sf.openrocket.simulation.FlightData#getFlightTime()}.
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*/
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@Test
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public void testGetFlightTime() {
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final double[] times = new double[] {
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1.0,
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5.0,
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15.0,
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20.1,
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30.2
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};
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FlightDataBranch branch =
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createFlightDataBranch("Test Flight Time", FlightDataType.TYPE_TIME, times);
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// Flight time is calculated as the last time entry
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FlightData data = new FlightData(branch);
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assertEquals(30.2, data.getFlightTime(), 0.000);
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}
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/**
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* Test method for {@link net.sf.openrocket.simulation.FlightData#getGroundHitVelocity()}.
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*/
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@Test
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public void testGetGroundHitVelocity() {
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/*
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* Setup a flight profile where there is data logged for every second.
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* The time events will start at 1, rather than 0 so the time into the
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* data log is the index + 1.0 seconds.
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*
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* i.e. at second 1, the velocity becomes 1.2 m/s, the altitude of the
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* rocket is 1.2, and the LiftOff event is saved.
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*
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* This loosely approximates a flight of about 21 seconds where it
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* flies up quickly and comes down quickly. The actual flight profile
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* is not as important as the fact that a profile exists.
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*
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* Each array is stored as
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*/
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final double[] velocities = new double[] {
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// launch to burn out
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1.2, 15.0, 31.1, 45.6,
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// burn out to apogee
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33.6, 21.2, 14.1, 6.8, 0.0,
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// apogee to ejection charge
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2.4, 4.7, 8.6, 9.23,
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// ejection charge to parachute deployment
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7.1, 6.2, 6.2, 6.2, 6.2,
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// parachute deployment to ground hit
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6.2, 0.0, 0.0
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};
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final double[] altitudes = new double[] {
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// launch to burn out
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1.2, 16.2, 47.3, 92.9,
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// burn out to apogee
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126.5, 147.7, 161.8, 168.6, 168.6,
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// apogee to ejection charge
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166.2, 161.5, 152.9, 143.67,
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// ejection charge to parachute deployment
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136.57, 113.81, 91.05, 68.29, 45.53,
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// parachute deployment to ground hit
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22.77, 0.0, 0.0
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};
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final FlightEvent.Type[] eventTypes = new FlightEvent.Type[] {
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// launch to burn out
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FlightEvent.Type.LIFTOFF, FlightEvent.Type.LAUNCHROD,
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FlightEvent.Type.ALTITUDE, FlightEvent.Type.BURNOUT,
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// burn out to apogee
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FlightEvent.Type.ALTITUDE, FlightEvent.Type.ALTITUDE,
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FlightEvent.Type.ALTITUDE, FlightEvent.Type.ALTITUDE,
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FlightEvent.Type.APOGEE,
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// apogee to ejection charge
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FlightEvent.Type.ALTITUDE, FlightEvent.Type.ALTITUDE,
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FlightEvent.Type.ALTITUDE, FlightEvent.Type.EJECTION_CHARGE,
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// ejection charge to parachute deployment
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FlightEvent.Type.ALTITUDE, FlightEvent.Type.RECOVERY_DEVICE_DEPLOYMENT,
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FlightEvent.Type.ALTITUDE, FlightEvent.Type.ALTITUDE,
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FlightEvent.Type.ALTITUDE,
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// parachute deployment to ground hit
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FlightEvent.Type.GROUND_HIT, FlightEvent.Type.ALTITUDE,
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FlightEvent.Type.SIMULATION_END
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};
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assertEquals(velocities.length, eventTypes.length);
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assertEquals(velocities.length, altitudes.length);
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// This flight data branch only needs to record for time,
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// altitude and velocity.
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FlightDataBranch branch =
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new FlightDataBranch("Ground Hit Velocities",
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FlightDataType.TYPE_TIME,
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FlightDataType.TYPE_ALTITUDE,
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FlightDataType.TYPE_VELOCITY_TOTAL);
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for (int i = 0; i < velocities.length; i++) {
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branch.addPoint();
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// the data entries are 1 second ahead of the index
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double time = i + 1.0;
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branch.setValue(FlightDataType.TYPE_TIME, time);
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branch.setValue(FlightDataType.TYPE_ALTITUDE, altitudes[i]);
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branch.setValue(FlightDataType.TYPE_VELOCITY_TOTAL, velocities[i]);
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branch.addEvent(new FlightEvent(eventTypes[i], time));
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}
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FlightData data = new FlightData(branch);
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assertEquals(6.2, data.getGroundHitVelocity(), 0.000);
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}
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}
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