3 Commits

Author SHA1 Message Date
35743c64b6 Finish AB4 2022-04-27 23:29:24 +02:00
b3ddcec038 Fix error in JavaDoc 2022-04-27 19:03:09 +02:00
cf188f1b2d Refactor for AB4 2022-04-27 19:00:45 +02:00
12 changed files with 388 additions and 244 deletions

View File

@@ -61,5 +61,3 @@ Himmelskörpern:
- Implementierung von `BodyForceMap`: 2 Punkte
- Anpassung von `Simulation`: 1 Punkt
- Gesamt: 5 Punkte

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@@ -47,4 +47,3 @@ Allgemeiner Hinweis: bei einigen Methoden sind Vorbedingungen (_pre-conditions_)
- Implementierung von `BodyForceTreeMap`: 2 Punkte
- Implementierung von `Simulation3`: 1 Punkt
- Gesamt: 5 Punkte

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@@ -106,7 +106,7 @@ wird. Sie dürfen hier keine Typumwandlungen (Casts) und auch nicht die Methoden
- Es ist möglich, aber nicht verlangt, `addForceTo(CosmicSystem cs)` ohne Verwendung von
`getBodies()` zu implementieren. Dazu kann in `addForceTo(CosmicSystem cs)` der Zugriff auf
die eizelnen Körper in `cs` dadurch erreicht werden, dass `this` für alle seine Himmelskörper
die einzelnen Körper in `cs` dadurch erreicht werden, dass `this` für alle seine Himmelskörper
und Untersysteme `addForceTo(cs)` aufruft. Wird beim rekursiven Abstieg ein einzelner Himmelskörper
erreicht (Blattknoten) ruft dieser `cs.addForceFrom(this)` auf.
@@ -120,6 +120,3 @@ verändert wird, wenn `this` und `b` derselbe Himmelskörper sind.
- Implementierung von `Simulation4`: 1 Punkte
- Gesamt: 5 Punkte

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@@ -1,112 +1,74 @@
import java.util.ArrayList;
import java.util.Arrays;
import java.util.HashSet;
import org.junit.jupiter.api.Test;
import static org.junit.jupiter.api.Assertions.*;
public class Aufgabe4Test {
public static void main(String[] args) {
private NamedBodyForcePair sun2, mercury2, venus2, earth2, moon2, mars2, deimos2, phobos2, vesta2, pallas2, hygiea2, ceres2;
//TODO: uncomment for testing
/*
//test classes HierachicalSystem and NamedBodyForcePair
public void resetBodies() {
sun2 = new NamedBodyForcePair(SolSystem4.SUN_NAMED);
earth2 = new NamedBodyForcePair(SolSystem4.EARTH_NAMED);
moon2 = new NamedBodyForcePair(SolSystem4.MOON_NAMED);
mars2 = new NamedBodyForcePair(SolSystem4.MARS_NAMED);
deimos2 = new NamedBodyForcePair(SolSystem4.DEIMOS_NAMED);
phobos2 = new NamedBodyForcePair(SolSystem4.PHOBOS_NAMED);
mercury2 = new NamedBodyForcePair(SolSystem4.MERCURY_NAMED);
venus2 = new NamedBodyForcePair(SolSystem4.VENUS_NAMED);
vesta2 = new NamedBodyForcePair(SolSystem4.VESTA_NAMED);
pallas2 = new NamedBodyForcePair(SolSystem4.PALLAS_NAMED);
hygiea2 = new NamedBodyForcePair(SolSystem4.HYGIEA_NAMED);
ceres2 = new NamedBodyForcePair(SolSystem4.CERES_NAMED);
}
// create 12 bodies
Body sun1, earth1, moon1, mars1, deimos1, phobos1, mercury1, venus1, vesta1, pallas1,
hygiea1, ceres1;
NamedBodyForcePair sun2, mercury2, venus2, earth2, moon2, mars2, deimos2, phobos2, vesta2,
pallas2, hygiea2, ceres2;
@Test
public void testEP2() {
//test classes HierarchicalSystem and NamedBodyForcePair
sun1 = new Body(1.989E30, new Vector3(0.0,0.0,0.0), new Vector3(0.0,0.0,
0.0));
earth1 = new Body(5.972E24, new Vector3(-6.13135922534815E10,-1.383789852227691E11,
2.719682263474911E7), new Vector3(26832.720535473603,-11948.23168764519,1.9948243075997851));
moon1 = new Body(7.349E22, new Vector3(-6.132484773775896E10,-1.387394951280871E11,
1.701046736294776E7), new Vector3(27916.62329282941,-12020.39526008238,-94.89703264508708));
mars1 = new Body(6.41712E23, new Vector3(-1.7923193702925848E11,1.726665823982123E11
,7.991673845249474E9), new Vector3(-15925.78496403673,-15381.16179928219,68.67560910598857));
deimos1 = new Body(1.8E20, new Vector3(-1.792255010450533E11,1.726891122683271E11,
7.990659337380297E9), new Vector3(-17100.476719804457,-15020.348656808,631.2927851249581));
phobos1 = new Body(1.08E20, new Vector3(-1.792253482539647E11,1.72661109673625E11,
7.987848354800322E9), new Vector3(-14738.203714241401,-13671.17675223948,-411.0012490555253));
mercury1 = new Body(3.301E23, new Vector3(-5.167375560011926E10,
-4.217574885682655E10,1.14808913958168E9), new Vector3(21580.25398577148,-34951.03632847389,-4835.225596525241));
venus1 = new Body(4.86747E24, new Vector3(-3.123150865740532E10,
1.0395568504115701E11,3.173401325838074E9), new Vector3(-33748.180519629335,-10014.25141045021,1809.94488874165));
vesta1 = new Body(2.5908E20, new Vector3(-3.337493557929893E11,
-4.7147908276077385E10,4.1923010146878105E10), new Vector3(4440.54247538484,-19718.49074006637,48.06573124543601));
pallas1 = new Body(2.14E20, new Vector3(4.3452066613895575E11,-2.057319365171432E11,
1.0549957423213101E11), new Vector3(5058.947582097117,11184.45711782372,-8183.524138259704));
hygiea1 = new Body(8.32E19, new Vector3(-3.983943433707043E11,2.325833000024021E11,
-2.233667695713672E10), new Vector3(-6931.864585548552,-15686.8108598699,-690.5791992347208));
ceres1 = new Body(9.394E20, new Vector3(3.781372641419032E11,1.96718960466285E11,
-6.366459168068592E10), new Vector3(-8555.324226752316,14718.33755980907,2040.230135060142));
Body sun1 = new Body(SolSystem4.SUN);
Body earth1 = new Body(SolSystem4.EARTH);
Body moon1 = new Body(SolSystem4.MOON);
Body mars1 = new Body(SolSystem4.MARS);
Body deimos1 = new Body(SolSystem4.DEIMOS);
Body phobos1 = new Body(SolSystem4.PHOBOS);
Body mercury1 = new Body(SolSystem4.MERCURY);
Body venus1 = new Body(SolSystem4.VENUS);
Body vesta1 = new Body(SolSystem4.VESTA);
Body pallas1 = new Body(SolSystem4.PALLAS);
Body hygiea1 = new Body(SolSystem4.HYGIEA);
Body ceres1 = new Body(SolSystem4.CERES);
Body[] bodies = new Body[]{sun1, mercury1, venus1, earth1, moon1, mars1, deimos1, phobos1,
vesta1, pallas1, hygiea1, ceres1};
Body[] bodies = new Body[]{sun1, mercury1, venus1, earth1, moon1, mars1, deimos1, phobos1, vesta1, pallas1, hygiea1, ceres1};
Vector3[] forceOnBody = new Vector3[bodies.length];
resetBodies();
NamedBodyForcePair[] pairs = new NamedBodyForcePair[]{sun2, mercury2, venus2, earth2, moon2, mars2, deimos2, phobos2, vesta2, pallas2, hygiea2, ceres2};
// create the same 12 named body-force pairs
sun2 = new NamedBodyForcePair("Sun",1.989E30, new Vector3(0.0,0.0,0.0)
, new Vector3(0.0,0.0,0.0));
earth2 = new NamedBodyForcePair("Earth",5.972E24,
new Vector3(-6.13135922534815E10,-1.383789852227691E11,2.719682263474911E7), new Vector3(26832.720535473603,-11948.23168764519,1.9948243075997851));
moon2 = new NamedBodyForcePair("Moon",7.349E22,
new Vector3(-6.132484773775896E10,-1.387394951280871E11,1.701046736294776E7), new Vector3(27916.62329282941,-12020.39526008238,-94.89703264508708));
mars2 = new NamedBodyForcePair("Mars",6.41712E23,
new Vector3(-1.7923193702925848E11,1.726665823982123E11,7.991673845249474E9), new Vector3(-15925.78496403673,-15381.16179928219,68.67560910598857));
deimos2 = new NamedBodyForcePair("Deimos",1.8E20,
new Vector3(-1.792255010450533E11,1.726891122683271E11,7.990659337380297E9), new Vector3(-17100.476719804457,-15020.348656808,631.2927851249581));
phobos2 = new NamedBodyForcePair("Phobos",1.08E20,
new Vector3(-1.792253482539647E11,1.72661109673625E11,7.987848354800322E9), new Vector3(-14738.203714241401,-13671.17675223948,-411.0012490555253));
mercury2 = new NamedBodyForcePair("Mercury",3.301E23,
new Vector3(-5.167375560011926E10,-4.217574885682655E10,1.14808913958168E9), new Vector3(21580.25398577148,-34951.03632847389,-4835.225596525241));
venus2 = new NamedBodyForcePair("Venus",4.86747E24,
new Vector3(-3.123150865740532E10,1.0395568504115701E11,3.173401325838074E9), new Vector3(-33748.180519629335,-10014.25141045021,1809.94488874165));
vesta2 = new NamedBodyForcePair("Vesta",2.5908E20,
new Vector3(-3.337493557929893E11,-4.7147908276077385E10,4.1923010146878105E10), new Vector3(4440.54247538484,-19718.49074006637,48.06573124543601));
pallas2 = new NamedBodyForcePair("Pallas",2.14E20,
new Vector3(4.3452066613895575E11,-2.057319365171432E11,1.0549957423213101E11), new Vector3(5058.947582097117,11184.45711782372,-8183.524138259704));
hygiea2 = new NamedBodyForcePair("Hygiea",8.32E19,
new Vector3(-3.983943433707043E11,2.325833000024021E11,-2.233667695713672E10), new Vector3(-6931.864585548552,-15686.8108598699,-690.5791992347208));
ceres2 = new NamedBodyForcePair("Ceres",9.394E20,
new Vector3(3.781372641419032E11,1.96718960466285E11,-6.366459168068592E10), new Vector3(-8555.324226752316,14718.33755980907,2040.230135060142));
NamedBodyForcePair[] pairs = new NamedBodyForcePair[] {sun2, mercury2, venus2, earth2,
moon2, mars2, deimos2, phobos2,
vesta2, pallas2, hygiea2, ceres2};
// check basic functions of 'HierachicalSystem'
System.out.println("Test1:");
// check basic functions of 'HierarchicalSystem'
CosmicSystem earthSystem = new HierarchicalSystem(earth2, moon2);
CosmicSystem marsSystem = new HierarchicalSystem(mars2, deimos2, phobos2);
CosmicSystem solarSystem = new HierarchicalSystem(sun2, mercury2, venus2, earthSystem,
marsSystem, vesta2, pallas2, hygiea2, ceres2);
CosmicSystem solarSystem = new HierarchicalSystem(sun2, mercury2, venus2, earthSystem, marsSystem, vesta2, pallas2, hygiea2, ceres2);
testValue(earthSystem.numberOfBodies(), 2);
testValue(solarSystem.numberOfBodies(), 12);
assertEquals(2, earthSystem.numberOfBodies());
assertEquals(12, solarSystem.numberOfBodies());
System.out.println("Test2:");
System.out.println(solarSystem.toString());
testValue(solarSystem.toString().contains("Mars"), true);
testValue(solarSystem.toString().contains("Deimos"), true);
testValue(solarSystem.toString().contains("Moon"), true);
testValue(earthSystem.toString().contains("Moon"), true);
testValue(earthSystem.toString().contains("Earth"), true);
System.out.println(solarSystem);
assertTrue(solarSystem.toString().contains("Mars"));
assertTrue(solarSystem.toString().contains("Deimos"));
assertTrue(solarSystem.toString().contains("Moon"));
assertTrue(earthSystem.toString().contains("Moon"));
assertTrue(earthSystem.toString().contains("Earth"));
System.out.println("Test3:");
testValue(solarSystem.getMass(),1.9890118865556799E30);
assertEquals(1.9890118865556799E30, solarSystem.getMass());
System.out.println("Test4:");
BodyLinkedList bl = solarSystem.getBodies();
testValue(bl.size(),12);
assertEquals(12, bl.size());
HashSet<Body> set = new HashSet<>();
while(bl.size() > 0) {
while (bl.size() > 0) {
set.add(bl.pollFirst());
}
testValue(set.size(), 12);
assertEquals(12, set.size());
System.out.println("Test5:");
for (int seconds = 0; seconds < 50000; seconds++) {
// for each body (with index i): compute the total force exerted on it.
for (int i = 0; i < bodies.length; i++) {
@@ -129,41 +91,12 @@ public class Aufgabe4Test {
}
for (int i = 0; i < bodies.length; i++) {
testValue(bodies[i].massCenter().distanceTo(pairs[i].getMassCenter()),0);
assertEquals(0, bodies[i].massCenter().distanceTo(pairs[i].getMassCenter()));
}
System.out.println("Test6:");
sun2 = new NamedBodyForcePair("Sun",1.989E30, new Vector3(0.0,0.0,0.0)
, new Vector3(0.0,0.0,0.0));
earth2 = new NamedBodyForcePair("Earth",5.972E24,
new Vector3(-6.13135922534815E10,-1.383789852227691E11,2.719682263474911E7), new Vector3(26832.720535473603,-11948.23168764519,1.9948243075997851));
moon2 = new NamedBodyForcePair("Moon",7.349E22,
new Vector3(-6.132484773775896E10,-1.387394951280871E11,1.701046736294776E7), new Vector3(27916.62329282941,-12020.39526008238,-94.89703264508708));
mars2 = new NamedBodyForcePair("Mars",6.41712E23,
new Vector3(-1.7923193702925848E11,1.726665823982123E11,7.991673845249474E9), new Vector3(-15925.78496403673,-15381.16179928219,68.67560910598857));
deimos2 = new NamedBodyForcePair("Deimos",1.8E20,
new Vector3(-1.792255010450533E11,1.726891122683271E11,7.990659337380297E9), new Vector3(-17100.476719804457,-15020.348656808,631.2927851249581));
phobos2 = new NamedBodyForcePair("Phobos",1.08E20,
new Vector3(-1.792253482539647E11,1.72661109673625E11,7.987848354800322E9), new Vector3(-14738.203714241401,-13671.17675223948,-411.0012490555253));
mercury2 = new NamedBodyForcePair("Mercury",3.301E23,
new Vector3(-5.167375560011926E10,-4.217574885682655E10,1.14808913958168E9), new Vector3(21580.25398577148,-34951.03632847389,-4835.225596525241));
venus2 = new NamedBodyForcePair("Venus",4.86747E24,
new Vector3(-3.123150865740532E10,1.0395568504115701E11,3.173401325838074E9), new Vector3(-33748.180519629335,-10014.25141045021,1809.94488874165));
vesta2 = new NamedBodyForcePair("Vesta",2.5908E20,
new Vector3(-3.337493557929893E11,-4.7147908276077385E10,4.1923010146878105E10), new Vector3(4440.54247538484,-19718.49074006637,48.06573124543601));
pallas2 = new NamedBodyForcePair("Pallas",2.14E20,
new Vector3(4.3452066613895575E11,-2.057319365171432E11,1.0549957423213101E11), new Vector3(5058.947582097117,11184.45711782372,-8183.524138259704));
hygiea2 = new NamedBodyForcePair("Hygiea",8.32E19,
new Vector3(-3.983943433707043E11,2.325833000024021E11,-2.233667695713672E10), new Vector3(-6931.864585548552,-15686.8108598699,-690.5791992347208));
ceres2 = new NamedBodyForcePair("Ceres",9.394E20,
new Vector3(3.781372641419032E11,1.96718960466285E11,-6.366459168068592E10), new Vector3(-8555.324226752316,14718.33755980907,2040.230135060142));
pairs = new NamedBodyForcePair[] {sun2, mercury2, venus2, earth2,
moon2, mars2, deimos2, phobos2,
vesta2, pallas2, hygiea2, ceres2};
HierarchicalSystem hs = new HierarchicalSystem(sun2, mercury2, venus2,
new HierarchicalSystem(earth2, moon2), new HierarchicalSystem(mars2, deimos2,
phobos2), vesta2, pallas2, hygiea2, ceres2);
resetBodies();
pairs = new NamedBodyForcePair[]{sun2, mercury2, venus2, earth2, moon2, mars2, deimos2, phobos2, vesta2, pallas2, hygiea2, ceres2};
HierarchicalSystem hs = new HierarchicalSystem(sun2, mercury2, venus2, new HierarchicalSystem(earth2, moon2), new HierarchicalSystem(mars2, deimos2, phobos2), vesta2, pallas2, hygiea2, ceres2);
for (int seconds = 0; seconds < 50000; seconds++) {
hs.addForceTo(hs);
@@ -171,35 +104,7 @@ public class Aufgabe4Test {
}
for (int i = 0; i < bodies.length; i++) {
testValue(bodies[i].massCenter().distanceTo(pairs[i].getMassCenter()),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, bodies[i].massCenter().distanceTo(pairs[i].getMassCenter()));
}
}
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);
}
}
}

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@@ -35,8 +35,10 @@ public class Body {
* Hint: see simulation loop in Simulation.java to find out how this is done.
*/
public Vector3 gravitationalForce(Body b) {
if (b == this) return new Vector3();
Vector3 direction = b.massCenter.minus(massCenter);
double distance = direction.length();
if (distance == 0) return new Vector3();
direction.normalize();
double force = Simulation.G * mass * b.mass / (distance * distance);
return direction.times(force);
@@ -76,6 +78,10 @@ public class Body {
return mass;
}
public Vector3 massCenter() {
return massCenter;
}
public boolean collidesWith(Body body) {
return this.distanceTo(body) < this.radius() + body.radius();
}

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@@ -1,41 +1,59 @@
// A representation of a system of bodies with associated forces. Provides methods
// for computing current mutual forces, updating the positions of bodies and drawing
// the bodies in a CodeDraw object.
//
/**
* A representation of a system of bodies with associated forces. Provides methods
* for computing current mutual forces, updating the positions of bodies and drawing
* the bodies in a CodeDraw object.
*/
public interface CosmicSystem extends Drawable {
// Returns a readable representation of this system.
/**
* Returns a readable representation of this system.
*/
String toString();
// Returns the mass center of this system.
/**
* Returns the mass center of this system.
*/
Vector3 getMassCenter();
// Returns the overall mass of this system.
/**
* Returns the overall mass of this system.
*/
double getMass();
// Returns the overall number of bodies contained in this system.
/**
* Returns the overall number of bodies contained in this system.
*/
int numberOfBodies();
// Returns the distance between the mass centers of 'this' and the specified system.
//Precondition: cs != null
/**
* Returns the distance between the mass centers of 'this' and the specified system.
* Precondition: cs != null
*/
double distanceTo(CosmicSystem cs);
// Adds the force that the specified body exerts on each of this systems bodies to each of this
// systems bodies.
// Precondition: b != null
/**
* Adds the force that the specified body exerts on each of this systems bodies to each of this
* systems bodies.
* Precondition: b != null
*/
void addForceFrom(Body b);
// Adds the force that this system exerts on each of the bodies of 'cs' to the bodies in 'cs'.
// For exact computations this means that for each body of 'this' its force on each body of
// 'cs' is added to this body of 'cs'.
// Precondition: cs != null
/**
* Adds the force that this system exerts on each of the bodies of 'cs' to the bodies in 'cs'.
* For exact computations this means that for each body of 'this' its force on each body of
* 'cs' is added to this body of 'cs'.
* Precondition: cs != null
*/
void addForceTo(CosmicSystem cs);
// Returns a list with all the bodies of 'this'. The order is not defined.
/**
* Returns a list with all the bodies of 'this'. The order is not defined.
*/
BodyLinkedList getBodies();
// Moves each of the bodies of 'this' according to the previously accumulated forces and
// resets all forces to zero.
/**
* Moves each of the bodies of 'this' according to the previously accumulated forces and
* resets all forces to zero.
*/
void update();
}

View File

@@ -1,10 +1,13 @@
import codedraw.CodeDraw;
// An object that can be drawn in a CodeDraw canvas.
//
/**
* An object that can be drawn in a CodeDraw canvas.
*/
public interface Drawable {
//draws the object into the canvas 'cd'
//Precondition: cd != null
/**
* draws the object into the canvas 'cd'
* Precondition: cd != null
*/
void draw(CodeDraw cd);
}

View File

@@ -1,14 +1,113 @@
// A cosmic system that is composed of a central named body (of type 'NamedBodyForcePair')
// and an arbitrary number of subsystems (of type 'HierarchicalSystem') in its orbit.
// This class implements 'CosmicSystem'.
//
public class HierarchicalSystem /* TODO: add clause */ {
import codedraw.CodeDraw;
// TODO: define missing parts of this class.
/**
* A cosmic system that is composed of a central named body (of type 'NamedBodyForcePair')
* and an arbitrary number of subsystems (of type 'CosmicSystem') in its orbit.
* This class implements 'CosmicSystem'.
*/
public class HierarchicalSystem implements CosmicSystem {
// Initializes this system with a name and a central body.
private final NamedBodyForcePair central;
private final CosmicSystem[] orbit;
private final CosmicSystem[] all;
/**
* Initializes this system with a name and a central body.
*/
public HierarchicalSystem(NamedBodyForcePair central, CosmicSystem... inOrbit) {
// TODO: implement constructor.
this.central = central;
this.orbit = inOrbit;
this.all = new CosmicSystem[this.orbit.length + 1];
this.all[0] = central;
System.arraycopy(this.orbit, 0, this.all, 1, this.orbit.length);
}
@Override
public Vector3 getMassCenter() {
double mass = this.getMass();
Vector3 massCenter = new Vector3();
for (CosmicSystem sys : all) {
massCenter.add(sys.getMassCenter().times(sys.getMass() / mass));
}
return massCenter;
}
@Override
public double getMass() {
double mass = 0;
for (CosmicSystem sys : all) {
mass += sys.getMass();
}
return mass;
}
@Override
public int numberOfBodies() {
int num = 0;
for (CosmicSystem sys : all) {
num += sys.numberOfBodies();
}
return num;
}
@Override
public double distanceTo(CosmicSystem cs) {
return this.getMassCenter().distanceTo(cs.getMassCenter());
}
@Override
public void addForceFrom(Body b) {
for (CosmicSystem sys : all) {
sys.addForceFrom(b);
}
}
@Override
public void addForceTo(CosmicSystem cs) {
for (CosmicSystem sys : all) {
sys.addForceTo(cs);
}
}
@Override
public BodyLinkedList getBodies() {
BodyLinkedList list = new BodyLinkedList();
for (CosmicSystem sys : all) {
for (Body b : sys.getBodies()) {
list.addFirst(b);
}
}
return list;
}
@Override
public void update() {
for (CosmicSystem sys : all) {
sys.update();
}
}
@Override
public void draw(CodeDraw cd) {
for (CosmicSystem sys : all) {
sys.draw(cd);
}
}
@Override
public String toString() {
StringBuilder sb = new StringBuilder();
sb.append(central.getName());
sb.append(" {");
boolean first = true;
for (CosmicSystem sys : orbit) {
if (!first) sb.append(", ");
sb.append(sys.toString());
first = false;
}
sb.append("}");
return sb.toString();
}
}

View File

@@ -1,21 +1,93 @@
// A body with a name and an associated force. The leaf node of
// a hierarchical cosmic system. This class implements 'CosmicSystem'.
//
public class NamedBodyForcePair /* TODO: add clause */ {
import codedraw.CodeDraw;
// TODO: define missing parts of this class.
/**
* A body with a name and an associated force. The leaf node of
* a hierarchical cosmic system. This class implements 'CosmicSystem'.
*/
public class NamedBodyForcePair implements CosmicSystem {
// Initializes this with name, mass, current position and movement. The associated force
// is initialized with a zero vector.
private final String name;
private final Body body;
private final Vector3 force = new Vector3();
/**
* Initializes this with name, mass, current position and movement. The associated force
* is initialized with a zero vector.
*/
public NamedBodyForcePair(String name, double mass, Vector3 massCenter, Vector3 currentMovement) {
// TODO: implement constructor.
this(name, new Body(mass, massCenter, currentMovement));
}
// Returns the name of the body.
public String getName() {
// TODO: implement method.
return "";
public NamedBodyForcePair(String name, Body b) {
this.body = b;
this.name = name;
}
public NamedBodyForcePair(NamedBodyForcePair other) {
this(other.name, new Body(other.body));
}
public Body getBody() {
return body;
}
/**
* Returns the name of the body.
*/
public String getName() {
return name;
}
@Override
public String toString() {
return this.getName();
}
@Override
public Vector3 getMassCenter() {
return body.massCenter();
}
@Override
public double getMass() {
return body.mass();
}
@Override
public int numberOfBodies() {
return 1;
}
@Override
public double distanceTo(CosmicSystem cs) {
return getMassCenter().distanceTo(cs.getMassCenter());
}
@Override
public void addForceFrom(Body b) {
force.add(body.gravitationalForce(b));
}
@Override
public void addForceTo(CosmicSystem cs) {
cs.addForceFrom(body);
}
@Override
public BodyLinkedList getBodies() {
BodyLinkedList list = new BodyLinkedList();
list.addFirst(body);
return list;
}
@Override
public void update() {
body.move(force);
force.set(0);
}
@Override
public void draw(CodeDraw cd) {
body.draw(cd);
}
}

View File

@@ -2,52 +2,50 @@ import codedraw.CodeDraw;
import java.awt.*;
// Simulates the formation of a massive solar system.
//
/**
* Simulates the formation of a massive solar system.
*/
public class Simulation4 {
// gravitational constant
public static final double G = 6.6743e-11;
public static final double SECTION_SIZE = 10 * Simulation.AU;
// one astronomical unit (AU) is the average distance of earth to the sun.
public static final double AU = 150e9; // meters
// one light year
public static final double LY = 9.461e15; // meters
// some further constants needed in the simulation
public static final double SUN_MASS = 1.989e30; // kilograms
public static final double SUN_RADIUS = 696340e3; // meters
public static final double EARTH_MASS = 5.972e24; // kilograms
public static final double EARTH_RADIUS = 6371e3; // meters
// set some system parameters
public static final double SECTION_SIZE = 10 * AU; // the size of the square region in space
// all quantities are based on units of kilogram respectively second and meter.
// The main simulation method using instances of other classes.
/**
* The main simulation method using instances of other classes.
*/
public static void main(String[] args) {
// simulation
CodeDraw cd = new CodeDraw();
// create solar system with 12 bodies
NamedBodyForcePair sun = new NamedBodyForcePair("Sun",1.989E30, new Vector3(0.0,0.0,0.0), new Vector3(0.0,0.0,0.0));
NamedBodyForcePair earth = new NamedBodyForcePair("Earth",5.972E24, new Vector3(-6.13135922534815E10,-1.383789852227691E11,2.719682263474911E7), new Vector3(26832.720535473603,-11948.23168764519,1.9948243075997851));
NamedBodyForcePair moon = new NamedBodyForcePair("Moon",7.349E22, new Vector3(-6.132484773775896E10,-1.387394951280871E11,1.701046736294776E7), new Vector3(27916.62329282941,-12020.39526008238,-94.89703264508708));
NamedBodyForcePair mars = new NamedBodyForcePair("Mars",6.41712E23, new Vector3(-1.7923193702925848E11,1.726665823982123E11,7.991673845249474E9), new Vector3(-15925.78496403673,-15381.16179928219,68.67560910598857));
NamedBodyForcePair deimos = new NamedBodyForcePair("Deimos",1.8E20, new Vector3(-1.792255010450533E11,1.726891122683271E11,7.990659337380297E9), new Vector3(-17100.476719804457,-15020.348656808,631.2927851249581));
NamedBodyForcePair phobos = new NamedBodyForcePair("Phobos",1.08E20, new Vector3(-1.792253482539647E11,1.72661109673625E11,7.987848354800322E9), new Vector3(-14738.203714241401,-13671.17675223948,-411.0012490555253));
NamedBodyForcePair mercury = new NamedBodyForcePair("Mercury",3.301E23, new Vector3(-5.167375560011926E10,-4.217574885682655E10,1.14808913958168E9), new Vector3(21580.25398577148,-34951.03632847389,-4835.225596525241));
NamedBodyForcePair venus = new NamedBodyForcePair("Venus",4.86747E24, new Vector3(-3.123150865740532E10,1.0395568504115701E11,3.173401325838074E9), new Vector3(-33748.180519629335,-10014.25141045021,1809.94488874165));
NamedBodyForcePair vesta = new NamedBodyForcePair("Vesta",2.5908E20, new Vector3(-3.337493557929893E11,-4.7147908276077385E10,4.1923010146878105E10), new Vector3(4440.54247538484,-19718.49074006637,48.06573124543601));
NamedBodyForcePair pallas = new NamedBodyForcePair("Pallas",2.14E20, new Vector3(4.3452066613895575E11,-2.057319365171432E11,1.0549957423213101E11), new Vector3(5058.947582097117,11184.45711782372,-8183.524138259704));
NamedBodyForcePair hygiea = new NamedBodyForcePair("Hygiea",8.32E19, new Vector3(-3.983943433707043E11,2.325833000024021E11,-2.233667695713672E10), new Vector3(-6931.864585548552,-15686.8108598699,-690.5791992347208));
NamedBodyForcePair ceres = new NamedBodyForcePair("Ceres",9.394E20, new Vector3(3.781372641419032E11,1.96718960466285E11,-6.366459168068592E10), new Vector3(-8555.324226752316,14718.33755980907,2040.230135060142));
NamedBodyForcePair sun = new NamedBodyForcePair(SolSystem4.SUN_NAMED);
NamedBodyForcePair earth = new NamedBodyForcePair(SolSystem4.EARTH_NAMED);
NamedBodyForcePair moon = new NamedBodyForcePair(SolSystem4.MOON_NAMED);
NamedBodyForcePair mars = new NamedBodyForcePair(SolSystem4.MARS_NAMED);
NamedBodyForcePair deimos = new NamedBodyForcePair(SolSystem4.DEIMOS_NAMED);
NamedBodyForcePair phobos = new NamedBodyForcePair(SolSystem4.PHOBOS_NAMED);
NamedBodyForcePair mercury = new NamedBodyForcePair(SolSystem4.MERCURY_NAMED);
NamedBodyForcePair venus = new NamedBodyForcePair(SolSystem4.VENUS_NAMED);
NamedBodyForcePair vesta = new NamedBodyForcePair(SolSystem4.VESTA_NAMED);
NamedBodyForcePair pallas = new NamedBodyForcePair(SolSystem4.PALLAS_NAMED);
NamedBodyForcePair hygiea = new NamedBodyForcePair(SolSystem4.HYGIEA_NAMED);
NamedBodyForcePair ceres = new NamedBodyForcePair(SolSystem4.CERES_NAMED);
//TODO: implementation of this method according to 'Aufgabenblatt4.md'.
CosmicSystem earthSystem = new HierarchicalSystem(earth, moon);
CosmicSystem marsSystem = new HierarchicalSystem(mars, deimos, phobos);
CosmicSystem sol = new HierarchicalSystem(sun, mercury, venus, earthSystem, marsSystem, vesta, pallas, hygiea, ceres);
long seconds = 0;
while (true) {
seconds++;
for (Body b : sol.getBodies()) {
sol.addForceFrom(b);
}
sol.update();
if ((seconds % 3600) == 0) {
cd.clear(Color.BLACK);
sol.draw(cd);
cd.show();
}
}
}
}

27
src/SolSystem4.java Normal file
View File

@@ -0,0 +1,27 @@
public class SolSystem4 {
public static final Body SUN = new Body(1.989E30, new Vector3(0.0, 0.0, 0.0), new Vector3(0.0, 0.0, 0.0));
public static final Body EARTH = new Body(5.972E24, new Vector3(-6.13135922534815E10, -1.383789852227691E11, 2.719682263474911E7), new Vector3(26832.720535473603, -11948.23168764519, 1.9948243075997851));
public static final Body MOON = new Body(7.349E22, new Vector3(-6.132484773775896E10, -1.387394951280871E11, 1.701046736294776E7), new Vector3(27916.62329282941, -12020.39526008238, -94.89703264508708));
public static final Body MARS = new Body(6.41712E23, new Vector3(-1.7923193702925848E11, 1.726665823982123E11, 7.991673845249474E9), new Vector3(-15925.78496403673, -15381.16179928219, 68.67560910598857));
public static final Body DEIMOS = new Body(1.8E20, new Vector3(-1.792255010450533E11, 1.726891122683271E11, 7.990659337380297E9), new Vector3(-17100.476719804457, -15020.348656808, 631.2927851249581));
public static final Body PHOBOS = new Body(1.08E20, new Vector3(-1.792253482539647E11, 1.72661109673625E11, 7.987848354800322E9), new Vector3(-14738.203714241401, -13671.17675223948, -411.0012490555253));
public static final Body MERCURY = new Body(3.301E23, new Vector3(-5.167375560011926E10, -4.217574885682655E10, 1.14808913958168E9), new Vector3(21580.25398577148, -34951.03632847389, -4835.225596525241));
public static final Body VENUS = new Body(4.86747E24, new Vector3(-3.123150865740532E10, 1.0395568504115701E11, 3.173401325838074E9), new Vector3(-33748.180519629335, -10014.25141045021, 1809.94488874165));
public static final Body VESTA = new Body(2.5908E20, new Vector3(-3.337493557929893E11, -4.7147908276077385E10, 4.1923010146878105E10), new Vector3(4440.54247538484, -19718.49074006637, 48.06573124543601));
public static final Body PALLAS = new Body(2.14E20, new Vector3(4.3452066613895575E11, -2.057319365171432E11, 1.0549957423213101E11), new Vector3(5058.947582097117, 11184.45711782372, -8183.524138259704));
public static final Body HYGIEA = new Body(8.32E19, new Vector3(-3.983943433707043E11, 2.325833000024021E11, -2.233667695713672E10), new Vector3(-6931.864585548552, -15686.8108598699, -690.5791992347208));
public static final Body CERES = new Body(9.394E20, new Vector3(3.781372641419032E11, 1.96718960466285E11, -6.366459168068592E10), new Vector3(-8555.324226752316, 14718.33755980907, 2040.230135060142));
public static final NamedBodyForcePair SUN_NAMED = new NamedBodyForcePair("Sun", SUN);
public static final NamedBodyForcePair EARTH_NAMED = new NamedBodyForcePair("Earth", EARTH);
public static final NamedBodyForcePair MOON_NAMED = new NamedBodyForcePair("Moon", MOON);
public static final NamedBodyForcePair MARS_NAMED = new NamedBodyForcePair("Mars", MARS);
public static final NamedBodyForcePair DEIMOS_NAMED = new NamedBodyForcePair("Deimos", DEIMOS);
public static final NamedBodyForcePair PHOBOS_NAMED = new NamedBodyForcePair("Phobos", PHOBOS);
public static final NamedBodyForcePair MERCURY_NAMED = new NamedBodyForcePair("Mercury", MERCURY);
public static final NamedBodyForcePair VENUS_NAMED = new NamedBodyForcePair("Venus", VENUS);
public static final NamedBodyForcePair VESTA_NAMED = new NamedBodyForcePair("Vesta", VESTA);
public static final NamedBodyForcePair PALLAS_NAMED = new NamedBodyForcePair("Pallas", PALLAS);
public static final NamedBodyForcePair HYGIEA_NAMED = new NamedBodyForcePair("Hygiea", HYGIEA);
public static final NamedBodyForcePair CERES_NAMED = new NamedBodyForcePair("Ceres", CERES);
}

View File

@@ -26,6 +26,16 @@ public class Vector3 {
this(other.x, other.y, other.z);
}
public void set(double v) {
set(v, v, v);
}
public void set(double x, double y, double z) {
this.x = x;
this.y = y;
this.z = z;
}
/**
* Returns the sum of this vector and vector 'v'.
*/
@@ -33,6 +43,12 @@ public class Vector3 {
return new Vector3(x + v.x, y + v.y, z + v.z);
}
public void add(Vector3 v) {
this.x += v.x;
this.y += v.y;
this.z += v.z;
}
/**
* Returns the product of this vector and 'd'.
*/
@@ -47,6 +63,12 @@ public class Vector3 {
return new Vector3(x - v.x, y - v.y, z - v.z);
}
public void sub(Vector3 v) {
this.x -= v.x;
this.y -= v.y;
this.z -= v.z;
}
/**
* Returns the Euclidean distance of this vector
* to the specified vector 'v'.
@@ -77,11 +99,11 @@ public class Vector3 {
}
public double getScreenX(CodeDraw cd) {
return cd.getWidth() * (this.x + Simulation.SECTION_SIZE / 2) / Simulation.SECTION_SIZE;
return cd.getWidth() * (this.x + Simulation4.SECTION_SIZE / 2) / Simulation4.SECTION_SIZE;
}
public double getScreenY(CodeDraw cd) {
return cd.getWidth() * (this.y + Simulation.SECTION_SIZE / 2) / Simulation.SECTION_SIZE;
return cd.getWidth() * (this.y + Simulation4.SECTION_SIZE / 2) / Simulation4.SECTION_SIZE;
}
/**
@@ -89,7 +111,7 @@ public class Vector3 {
* in the canvas associated with 'cd'. The z-coordinate is not used.
*/
public void drawAsFilledCircle(CodeDraw cd, double radius) {
radius = cd.getWidth() * radius / Simulation.SECTION_SIZE;
radius = cd.getWidth() * radius / Simulation4.SECTION_SIZE;
cd.fillCircle(getScreenX(cd), getScreenY(cd), Math.max(radius, 1.5));
}