update unit tests

This commit is contained in:
JoePfeiffer 2023-03-09 15:56:59 -07:00
parent 68bdd7ff2c
commit 435b2bfcad
3 changed files with 89 additions and 39 deletions

View File

@ -1104,6 +1104,26 @@ public class TestRockets {
return rocket;
}
// Several simulations need the Falcon9Heavy, but with fins added to the
// core stage (without them, there is a simulation exception at stage separation
// This method is intended to add those fins to the F9H, but will in fact
// add them to the second stage of a rocket
public static void addCoreFins(Rocket rocket) {
final int bodyFinCount = 4;
final double bodyFinRootChord = 0.05;
final double bodyFinTipChord = bodyFinRootChord;
final double bodyFinHeight = 0.025;
final double bodyFinSweep = 0.0;
final AxialMethod bodyFinAxialMethod = AxialMethod.BOTTOM;
final double bodyFinAxialOffset = 0.0;
final TrapezoidFinSet finSet = new TrapezoidFinSet(bodyFinCount, bodyFinRootChord, bodyFinTipChord, bodyFinSweep, bodyFinHeight);
finSet.setName("Body Tube FinSet");
finSet.setAxialMethod(bodyFinAxialMethod);
rocket.getChild(1).getChild(0).addChild(finSet);
}
// This is a simple four-fin rocket with large endplates on the
// fins, for testing CG and CP calculations with fins on pods.
// not a complete rocket (no motor mount nor recovery system)

View File

@ -148,8 +148,12 @@ public class DisableStageTest extends BaseTestCase {
@Test
public void testBooster1() {
//// Test disabling the stage
Rocket rocketRemoved = TestRockets.makeFalcon9Heavy(); // Rocket with the last stage removed
TestRockets.addCoreFins(rocketRemoved);
Rocket rocketDisabled = TestRockets.makeFalcon9Heavy(); // Rocket with the last stage disabled
TestRockets.addCoreFins(rocketDisabled);
FlightConfigurationId fcid = new FlightConfigurationId(TestRockets.FALCON_9H_FCID_1);
int stageNr = 2; // Stage 2 is the Parallel Booster Stage
@ -171,6 +175,8 @@ public class DisableStageTest extends BaseTestCase {
//// Test re-enableing the stage.
Rocket rocketOriginal = TestRockets.makeFalcon9Heavy();
TestRockets.addCoreFins(rocketOriginal);
Simulation simOriginal = new Simulation(rocketOriginal);
simOriginal.setFlightConfigurationId(fcid);
simOriginal.getOptions().setISAAtmosphere(true);
@ -188,7 +194,10 @@ public class DisableStageTest extends BaseTestCase {
public void testBooster2() {
//// Test disabling the stage
Rocket rocketRemoved = TestRockets.makeFalcon9Heavy(); // Rocket with the last stage removed
TestRockets.addCoreFins(rocketRemoved);
Rocket rocketDisabled = TestRockets.makeFalcon9Heavy(); // Rocket with the last stage disabled
TestRockets.addCoreFins(rocketDisabled);
FlightConfigurationId fid = new FlightConfigurationId(TestRockets.FALCON_9H_FCID_1);
int stageNr = 1; // Stage 1 is the Parallel Booster Stage's parent stage
@ -225,6 +234,8 @@ public class DisableStageTest extends BaseTestCase {
//// Test re-enableing the stage.
Rocket rocketOriginal = TestRockets.makeFalcon9Heavy();
TestRockets.addCoreFins(rocketOriginal);
Simulation simOriginal = new Simulation(rocketOriginal);
simOriginal.setFlightConfigurationId(fid);
simOriginal.getOptions().setISAAtmosphere(true);

View File

@ -85,6 +85,8 @@ public class FlightEventsTest extends BaseTestCase {
@Test
public void testMultiStage() throws SimulationException {
final Rocket rocket = TestRockets.makeFalcon9Heavy();
TestRockets.addCoreFins(rocket);
final Simulation sim = new Simulation(rocket);
sim.getOptions().setISAAtmosphere(true);
sim.getOptions().setTimeStep(0.05);
@ -98,32 +100,49 @@ public class FlightEventsTest extends BaseTestCase {
final int branchCount = sim.getSimulatedData().getBranchCount();
assertEquals(" Multi-stage simulation invalid branch count", 3, branchCount);
final AxialStage coreStage = rocket.getStage(1);
final ParallelStage boosterStage = (ParallelStage) rocket.getStage(2);
final InnerTube boosterMotorTubes = (InnerTube) boosterStage.getChild(1).getChild(0);
final BodyTube coreBody = (BodyTube) coreStage.getChild(0);
// events whose time is too variable to check are given a time of 1200
for (int b = 0; b < 3; b++) {
final FlightEvent.Type[] expectedEventTypes;
final double[] expectedEventTimes;
FlightEvent[] expectedEvents;
final RocketComponent[] expectedSources;
switch (b) {
case 0:
expectedEventTypes = new FlightEvent.Type[]{FlightEvent.Type.LAUNCH, FlightEvent.Type.IGNITION, FlightEvent.Type.IGNITION,
FlightEvent.Type.LIFTOFF, FlightEvent.Type.LAUNCHROD, FlightEvent.Type.APOGEE,
FlightEvent.Type.BURNOUT, FlightEvent.Type.EJECTION_CHARGE, FlightEvent.Type.STAGE_SEPARATION,
FlightEvent.Type.BURNOUT, FlightEvent.Type.EJECTION_CHARGE, FlightEvent.Type.STAGE_SEPARATION,
FlightEvent.Type.TUMBLE, FlightEvent.Type.GROUND_HIT, FlightEvent.Type.SIMULATION_END};
expectedEventTimes = new double[]{0.0, 0.0, 0.0, 0.1225, 0.125, 1.735, 2.0, 2.0, 2.0, 2.0, 2.0, 2.0}; // Tumble and ground hit time are too variable, so don't include it
final AxialStage coreStage = rocket.getStage(1);
final ParallelStage boosterStage = (ParallelStage) rocket.getStage(2);
final InnerTube boosterMotorTubes = (InnerTube) boosterStage.getChild(1).getChild(0);
final BodyTube coreBody = (BodyTube) coreStage.getChild(0);
expectedSources = new RocketComponent[]{rocket, boosterMotorTubes, coreBody, null, null, rocket,
boosterMotorTubes, boosterStage, boosterStage, coreBody, coreStage, coreStage,
null, null, null};
expectedEvents = new FlightEvent[] {
new FlightEvent(FlightEvent.Type.LAUNCH, 0.0, rocket),
new FlightEvent(FlightEvent.Type.IGNITION, 0.0, boosterMotorTubes),
new FlightEvent(FlightEvent.Type.IGNITION, 0.0, coreBody),
new FlightEvent(FlightEvent.Type.LIFTOFF, 0.1225, null),
new FlightEvent(FlightEvent.Type.LAUNCHROD, 0.125, null),
new FlightEvent(FlightEvent.Type.APOGEE, 1.86, rocket),
new FlightEvent(FlightEvent.Type.BURNOUT, 2.0, boosterMotorTubes),
new FlightEvent(FlightEvent.Type.EJECTION_CHARGE, 2.0, boosterStage),
new FlightEvent(FlightEvent.Type.STAGE_SEPARATION, 2.0, boosterStage),
new FlightEvent(FlightEvent.Type.BURNOUT, 2.0, coreBody),
new FlightEvent(FlightEvent.Type.EJECTION_CHARGE, 2.0, coreStage),
new FlightEvent(FlightEvent.Type.STAGE_SEPARATION, 2.0, coreStage),
new FlightEvent(FlightEvent.Type.TUMBLE, 2.4127, null),
new FlightEvent(FlightEvent.Type.GROUND_HIT, 1200, null),
new FlightEvent(FlightEvent.Type.SIMULATION_END, 1200, null)
};
break;
case 1:
expectedEvents = new FlightEvent[] {
new FlightEvent(FlightEvent.Type.STAGE_SEPARATION, 2.0, coreStage),
new FlightEvent(FlightEvent.Type.GROUND_HIT, 1200, null),
new FlightEvent(FlightEvent.Type.SIMULATION_END, 1200, null)
};
break;
case 2:
expectedEventTypes = new FlightEvent.Type[]{FlightEvent.Type.TUMBLE, FlightEvent.Type.GROUND_HIT,
FlightEvent.Type.SIMULATION_END};
expectedEventTimes = new double[]{}; // Tumble and ground hit time are too variable, so don't include it
expectedSources = new RocketComponent[]{null, null, null};
expectedEvents = new FlightEvent[] {
new FlightEvent(FlightEvent.Type.STAGE_SEPARATION, 2.0, boosterStage),
new FlightEvent(FlightEvent.Type.TUMBLE, 3.551, null),
new FlightEvent(FlightEvent.Type.GROUND_HIT, 1200, null),
new FlightEvent(FlightEvent.Type.SIMULATION_END, 1200, null)
};
break;
default:
throw new IllegalStateException("Invalid branch number " + b);
@ -131,28 +150,28 @@ public class FlightEventsTest extends BaseTestCase {
// Test event count
final FlightDataBranch branch = sim.getSimulatedData().getBranch(b);
final List<FlightEvent> eventList = branch.getEvents();
final List<FlightEvent.Type> eventTypes = eventList.stream().map(FlightEvent::getType).collect(Collectors.toList());
assertEquals(" Multi-stage simulation, branch " + b + " invalid number of events", expectedEventTypes.length, eventTypes.size());
final FlightEvent[] events = (FlightEvent[]) branch.getEvents().toArray(new FlightEvent[0]);
for (int i = 0; i < events.length; i++) {
System.out.println("branch " + b + " index " + i + " event " + events[i]);
}
assertEquals(" Multi-stage simulation, branch " + b + " invalid number of events", expectedEvents.length, events.length);
// Test that all expected events are present, and in the right order
for (int i = 0; i < expectedEventTypes.length; i++) {
assertSame(" Flight type " + expectedEventTypes[i] + ", branch " + b + " not found in multi-stage simulation",
expectedEventTypes[i], eventTypes.get(i));
}
// Test that all expected events are present, in the right order, at the right time, from the right sources
for (int i = 0; i < events.length; i++) {
final FlightEvent expected = expectedEvents[i];
final FlightEvent actual = events[i];
assertSame("Branch " + b + " FlightEvent " + i + " type " + expected.getType() + " not found; FlightEvent " + actual.getType() + " found instead",
expected.getType(), actual.getType());
// Test that the event times are correct
for (int i = 0; i < expectedEventTimes.length; i++) {
assertEquals(" Flight type " + expectedEventTypes[i] + " has wrong time",
expectedEventTimes[i], eventList.get(i).getTime(), EPSILON);
}
if (1200 != expected.getTime()) {
assertEquals("Branch " + b + " FlightEvent " + i + " type " + expected.getType() + " has wrong time",
expected.getTime(), actual.getTime(), EPSILON);
}
// Test that the event sources are correct
for (int i = 0; i < expectedSources.length; i++) {
assertEquals(" Flight type " + expectedEventTypes[i] + " has wrong source",
expectedSources[i], eventList.get(i).getSource());
// Test that the event sources are correct
assertEquals("Branch " + b + " FlightEvent " + i + " type " + expected.getType() + " has wrong source",
expected.getSource(), actual.getSource());
}
}
}
}