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Refacotr code for AB8

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Lorenz Stechauner
2022-06-03 14:23:51 +02:00
parent 8f6320e069
commit cfba0106a9
10 changed files with 170 additions and 234 deletions
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4
angabe/Aufgabenblatt8.md
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@ -1,7 +1,7 @@
# Aufgabenblatt 8
## Allgemeine Anmerkungen
Ihre Lösung für dieses Aufgabenblatt ist bis Dienstag, 13.6., 11h durch `git commit` und `git push`
Ihre Lösung für dieses Aufgabenblatt ist bis Montag, 13.6., 11h durch `git commit` und `git push`
abzugeben.
Wenn Sie zusätzlich zu den gefragten Klassen und Interfaces weitere Klassen oder
Interfaces definieren, achten Sie darauf, dass die Klassennamen mit `My` beginnen, um Konflikte
@ -20,7 +20,7 @@ Validierung, Exceptions (S. 110-123).
- [states](../states) ist ein Verzeichnis, in dem mehrere Dateien mit der Endung `.txt`
mitgeliefert werden. Diese enthalten Daten von je einem Himmelskörper sowie dessen Positionen und
Geschwindigkeitsvektoren für alle Tage der Jahre 2019-2021. Die Angaben sind wie gewohnt in
kartesischen Koordinaten, wobei die Sonne den Urspung des Koordinatensystems bildet und die
kartesischen Koordinaten, wobei die Sonne den Ursprung des Koordinatensystems bildet und die
Ekliptik die x-y-Ebene darstellt. Die Daten stammen von [https://ssd.jpl.nasa.gov/horizons.cgi#top](https://ssd.jpl.nasa.gov/horizons.cgi#top).
**ACHTUNG**: Die Werte sind in km bzw. km/sec angegeben!

96
src/Aufgabe8Test.java
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@ -1,44 +1,29 @@
import org.junit.jupiter.api.Test;
import java.util.HashSet;
import java.util.NoSuchElementException;
import static org.junit.jupiter.api.Assertions.*;
public class Aufgabe8Test {
public static void main(String[] args) {
/* //TODO: uncomment for testing
@Test
public void testEP2() {
MassiveForceTreeMap map = new MassiveForceTreeMap();
NamedBody mars;
map.put(new NamedBody("Oumuamua", 8e6, new Vector3(0, 0, 0), new Vector3(0, 0, 0)),
new Vector3(0, 0, 0));
map.put(new NamedBody("Earth", 5.972E24, new Vector3(0, 0, 0), new Vector3(0, 0, 0)),
new Vector3(0, 0, 0));
map.put(new NamedBody("Moon", 7.349E22, new Vector3(0, 0, 0), new Vector3(0, 0, 0)),
new Vector3(0, 0, 0));
map.put(mars = new NamedBody("Mars", 6.41712E23, new Vector3(0, 0, 0),
new Vector3(0, 0, 0)),
new Vector3(0, 0, 0));
map.put(new NamedBody("Deimos", 1.8E20, new Vector3(0, 0, 0), new Vector3(0, 0, 0)),
new Vector3(0, 0, 0));
map.put(new NamedBody("Phobos", 1.08E20, new Vector3(0, 0, 0), new Vector3(0, 0, 0)),
new Vector3(0, 0, 0));
map.put(new NamedBody("Mercury", 3.301E23, new Vector3(0, 0, 0), new Vector3(0, 0, 0)),
new Vector3(0, 0, 0));
map.put(new NamedBody("Venus", 4.86747E24, new Vector3(0, 0, 0), new Vector3(0, 0, 0)),
new Vector3(0, 0, 0));
map.put(new NamedBody("Vesta", 2.5908E20, new Vector3(0, 0, 0), new Vector3(0, 0, 0)),
new Vector3(0, 0, 0));
map.put(new NamedBody("Pallas", 2.14E20, new Vector3(0, 0, 0), new Vector3(0, 0, 0)),
new Vector3(0, 0, 0));
map.put(new NamedBody("Hygiea", 8.32E19, new Vector3(0, 0, 0), new Vector3(0, 0, 0)),
new Vector3(0, 0, 0));
map.put(new NamedBody("Ceres", 9.394E20, new Vector3(0, 0, 0), new Vector3(0, 0, 0)),
new Vector3(0, 0, 0));
map.put(new NamedBody("Oumuamua", 8e6, new Vector3(), new Vector3()), new Vector3());
map.put(new NamedBody("Earth", 5.972E24, new Vector3(), new Vector3()), new Vector3());
map.put(new NamedBody("Moon", 7.349E22, new Vector3(), new Vector3()), new Vector3());
map.put(mars = new NamedBody("Mars", 6.41712E23, new Vector3(), new Vector3()), new Vector3());
map.put(new NamedBody("Deimos", 1.8E20, new Vector3(), new Vector3()), new Vector3());
map.put(new NamedBody("Phobos", 1.08E20, new Vector3(), new Vector3()), new Vector3());
map.put(new NamedBody("Mercury", 3.301E23, new Vector3(), new Vector3()), new Vector3());
map.put(new NamedBody("Venus", 4.86747E24, new Vector3(), new Vector3()), new Vector3());
map.put(new NamedBody("Vesta", 2.5908E20, new Vector3(), new Vector3()), new Vector3());
map.put(new NamedBody("Pallas", 2.14E20, new Vector3(), new Vector3()), new Vector3());
map.put(new NamedBody("Hygiea", 8.32E19, new Vector3(), new Vector3()), new Vector3());
map.put(new NamedBody("Ceres", 9.394E20, new Vector3(), new Vector3()), new Vector3());
System.out.println("Test1:");
MassiveIterator iterator = map.getKeys().iterator();
int count = 0;
while (iterator.hasNext()) {
@ -47,54 +32,17 @@ public class Aufgabe8Test {
}
count++;
}
testValue(count, 12);
testValue(map.getKeys().size(), 11);
testValue(map.getKeys().contains(mars), false);
assertEquals(12, count);
assertEquals(11, map.getKeys().size());
assertFalse(map.getKeys().contains(mars));
System.out.println("Test2:");
try {
iterator.next();
// this statement must not be reached
testValue(true, false);
} catch (NoSuchElementException e) {
testValue(true, true);
}
assertThrows(NoSuchElementException.class, iterator::next);
System.out.println("Test3:");
iterator = map.getKeys().iterator();
while (iterator.hasNext()) {
iterator.next();
iterator.remove();
}
testValue(map.getKeys().size(),0);
*/ //TODO: uncomment
}
public static void testComparison(Object first, Object second, boolean expected) {
boolean real = first == second;
if (real == expected) {
System.out.println("Successful comparison");
} else {
System.out.println("Comparison NOT successful! Expected value: " + expected + " / Given value: " + real);
assertEquals(0, map.getKeys().size());
}
}
public static void testValue(Object given, Object expected) {
if (given == expected) {
System.out.println("Successful test");
} else {
System.out.println("Test NOT successful! Expected value: " + expected + " / Given value: " + given);
}
}
public static void testValue(double given, double expected) {
if (given < expected + (expected + 1) / 1e12 && given > expected - (expected + 1) / 1e12) {
System.out.println("Successful test");
} else {
System.out.println("Test NOT successful! Expected value: " + expected + " / Given value: " + given);
}
}
}

37
src/ReadDataUtil.java
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@ -2,26 +2,25 @@ import java.io.*;
public class ReadDataUtil {
// Reads the position and velocity vector on the specified 'day' from the file with the
// specified 'path', and sets position and current velocity of 'b' accordingly. If
// successful the method returns 'true'. If the specified 'day' was not found in the file,
// 'b' is unchanged and the method returns 'false'.
// The file format is validated before reading the state.
// Lines before the line "$$SOE" and after the line "$$EOE" the are ignored. Each line of the
// file between the line "$$SOE" and the line "$$EOE" is required to have the following format:
// JDTDB, TIME, X, Y, Z, VX, VY, VZ
// where JDTDB is interpretable as a 'double' value, TIME is a string and X, Y, Z, VX, VY and
// VZ are interpretable as 'double' values. JDTDB can be ignored. The character ',' must only
// be used as field separator. If the file is not found, an exception of the class
// 'StateFileNotFoundException' is thrown. If it does not comply with the format described
// above, the method throws an exception of the class 'StateFileFormatException'. Both
// exceptions are subtypes of 'IOException'.
// Precondition: b != null, path != null, day != null and has the format YYYY-MM-DD.
public static boolean readConfiguration(NamedBody b, String path, String day)
throws IOException {
/**
* Reads the position and velocity vector on the specified 'day' from the file with the
* specified 'path', and sets position and current velocity of 'b' accordingly. If
* successful the method returns 'true'. If the specified 'day' was not found in the file,
* 'b' is unchanged and the method returns 'false'.
* The file format is validated before reading the state.
* Lines before the line "$$SOE" and after the line "$$EOE" the are ignored. Each line of the
* file between the line "$$SOE" and the line "$$EOE" is required to have the following format:
* JDTDB, TIME, X, Y, Z, VX, VY, VZ
* where JDTDB is interpretable as a 'double' value, TIME is a string and X, Y, Z, VX, VY and
* VZ are interpretable as 'double' values. JDTDB can be ignored. The character ',' must only
* be used as field separator. If the file is not found, an exception of the class
* 'StateFileNotFoundException' is thrown. If it does not comply with the format described
* above, the method throws an exception of the class 'StateFileFormatException'. Both
* exceptions are subtypes of 'IOException'.
* Precondition: b != null, path != null, day != null and has the format YYYY-MM-DD.
*/
public static boolean readConfiguration(NamedBody b, String path, String day) throws IOException {
// TODO: implement this method.
return false;
}
}

44
src/Simulation8.java
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@ -1,7 +1,8 @@
import codedraw.CodeDraw;
// Simulates the solar system.
//
/**
* Simulates the solar system.
*/
public class Simulation8 {
// gravitational constant
@ -24,37 +25,24 @@ public class Simulation8 {
// create solar system with 13 bodies
MassiveForceTreeMap map = new MassiveForceTreeMap();
map.put(new NamedBody("Oumuamua", 8e6, new Vector3(0, 0, 0), new Vector3(0, 0, 0)),
new Vector3(0, 0, 0));
map.put(new NamedBody("Earth", 5.972E24, new Vector3(0, 0, 0), new Vector3(0, 0, 0)),
new Vector3(0, 0, 0));
map.put(new NamedBody("Moon", 7.349E22, new Vector3(0, 0, 0), new Vector3(0, 0, 0)),
new Vector3(0, 0, 0));
map.put(new NamedBody("Mars1", 6.41712E23, new Vector3(0, 0, 0), new Vector3(0, 0, 0)),
new Vector3(0, 0, 0));
map.put(new NamedBody("Deimos", 1.8E20, new Vector3(0, 0, 0), new Vector3(0, 0, 0)),
new Vector3(0, 0, 0));
map.put(new NamedBody("Phobos", 1.08E20, new Vector3(0, 0, 0), new Vector3(0, 0, 0)),
new Vector3(0, 0, 0));
map.put(new NamedBody("Mercury", 3.301E23, new Vector3(0, 0, 0), new Vector3(0, 0, 0)),
new Vector3(0, 0, 0));
map.put(new NamedBody("Venus", 4.86747E24, new Vector3(0, 0, 0), new Vector3(0, 0, 0)),
new Vector3(0, 0, 0));
map.put(new NamedBody("Vesta", 2.5908E20, new Vector3(0, 0, 0), new Vector3(0, 0, 0)),
new Vector3(0, 0, 0));
map.put(new NamedBody("Pallas", 2.14E20, new Vector3(0, 0, 0), new Vector3(0, 0, 0)),
new Vector3(0, 0, 0));
map.put(new NamedBody("Hygiea", 8.32E19, new Vector3(0, 0, 0), new Vector3(0, 0, 0)),
new Vector3(0, 0, 0));
map.put(new NamedBody("Ceres1", 9.394E20, new Vector3(0, 0, 0), new Vector3(0, 0, 0)),
new Vector3(0, 0, 0));
map.put(new NamedBody("Oumuamua", 8e6, new Vector3(), new Vector3()), new Vector3());
map.put(new NamedBody("Earth", 5.972E24, new Vector3(), new Vector3()), new Vector3());
map.put(new NamedBody("Moon", 7.349E22, new Vector3(), new Vector3()), new Vector3());
map.put(new NamedBody("Mars1", 6.41712E23, new Vector3(), new Vector3()), new Vector3());
map.put(new NamedBody("Deimos", 1.8E20, new Vector3(), new Vector3()), new Vector3());
map.put(new NamedBody("Phobos", 1.08E20, new Vector3(), new Vector3()), new Vector3());
map.put(new NamedBody("Mercury", 3.301E23, new Vector3(), new Vector3()), new Vector3());
map.put(new NamedBody("Venus", 4.86747E24, new Vector3(), new Vector3()), new Vector3());
map.put(new NamedBody("Vesta", 2.5908E20, new Vector3(), new Vector3()), new Vector3());
map.put(new NamedBody("Pallas", 2.14E20, new Vector3(), new Vector3()), new Vector3());
map.put(new NamedBody("Hygiea", 8.32E19, new Vector3(), new Vector3()), new Vector3());
map.put(new NamedBody("Ceres1", 9.394E20, new Vector3(), new Vector3()), new Vector3());
//TODO: implementation of this method according to 'Aufgabenblatt8.md'.
// add sun after states have been read from files.
map.put(new NamedBody("Sun", 1.989E30, new Vector3(0, 0, 0), new Vector3(0, 0, 0)),
new Vector3(0, 0, 0));
map.put(new NamedBody("Sun", 1.989E30, new Vector3(), new Vector3()), new Vector3());
}
}

5
src/Simulation9.java
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@ -1,5 +1,6 @@
// Simulates the solar system.
//
/**
* Simulates the solar system.
*/
public class Simulation9 {
// TODO: Implement the simulation using the Java-Collections framework.