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Refactor AB6 Angabe

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Lorenz Stechauner
2022-05-17 17:28:26 +02:00
parent 2e14e45bb0
commit b89fc15602
8 changed files with 146 additions and 187 deletions
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40
src/Simulation6.java
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@@ -3,8 +3,9 @@ import codedraw.CodeDraw;
import java.awt.*;
import java.util.Random;
// Simulates the formation of a massive solar system.
//
/**
* Simulates the formation of a massive solar system.
*/
public class Simulation6 {
// gravitational constant
@@ -30,25 +31,26 @@ public class Simulation6 {
// 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
NamedBody sun = new NamedBody("Sun",1.989E30, new Vector3(0.0,0.0,0.0), new Vector3(0.0,0.0,0.0));
NamedBody earth = new NamedBody("Earth",5.972E24, new Vector3(-6.13135922534815E10,-1.383789852227691E11,2.719682263474911E7), new Vector3(26832.720535473603,-11948.23168764519,1.9948243075997851));
NamedBody moon = new NamedBody("Moon",7.349E22, new Vector3(-6.132484773775896E10,-1.387394951280871E11,1.701046736294776E7), new Vector3(27916.62329282941,-12020.39526008238,-94.89703264508708));
NamedBody mars = new NamedBody("Mars",6.41712E23, new Vector3(-1.7923193702925848E11,1.726665823982123E11,7.991673845249474E9), new Vector3(-15925.78496403673,-15381.16179928219,68.67560910598857));
NamedBody deimos = new NamedBody("Deimos",1.8E20, new Vector3(-1.792255010450533E11,1.726891122683271E11,7.990659337380297E9), new Vector3(-17100.476719804457,-15020.348656808,631.2927851249581));
NamedBody phobos = new NamedBody("Phobos",1.08E20, new Vector3(-1.792253482539647E11,1.72661109673625E11,7.987848354800322E9), new Vector3(-14738.203714241401,-13671.17675223948,-411.0012490555253));
NamedBody mercury = new NamedBody("Mercury",3.301E23, new Vector3(-5.167375560011926E10,-4.217574885682655E10,1.14808913958168E9), new Vector3(21580.25398577148,-34951.03632847389,-4835.225596525241));
NamedBody venus = new NamedBody("Venus",4.86747E24, new Vector3(-3.123150865740532E10,1.0395568504115701E11,3.173401325838074E9), new Vector3(-33748.180519629335,-10014.25141045021,1809.94488874165));
NamedBody vesta = new NamedBody("Vesta",2.5908E20, new Vector3(-3.337493557929893E11,-4.7147908276077385E10,4.1923010146878105E10), new Vector3(4440.54247538484,-19718.49074006637,48.06573124543601));
NamedBody pallas = new NamedBody("Pallas",2.14E20, new Vector3(4.3452066613895575E11,-2.057319365171432E11,1.0549957423213101E11), new Vector3(5058.947582097117,11184.45711782372,-8183.524138259704));
NamedBody hygiea = new NamedBody("Hygiea",8.32E19, new Vector3(-3.983943433707043E11,2.325833000024021E11,-2.233667695713672E10), new Vector3(-6931.864585548552,-15686.8108598699,-690.5791992347208));
NamedBody ceres = new NamedBody("Ceres",9.394E20, new Vector3(3.781372641419032E11,1.96718960466285E11,-6.366459168068592E10), new Vector3(-8555.324226752316,14718.33755980907,2040.230135060142));
NamedBody sun = new NamedBody(SolSystem4.SUN_NAMED);
NamedBody earth = new NamedBody(SolSystem4.EARTH_NAMED);
NamedBody moon = new NamedBody(SolSystem4.MOON_NAMED);
NamedBody mars = new NamedBody(SolSystem4.MARS_NAMED);
NamedBody deimos = new NamedBody(SolSystem4.DEIMOS_NAMED);
NamedBody phobos = new NamedBody(SolSystem4.PHOBOS_NAMED);
NamedBody mercury = new NamedBody(SolSystem4.MERCURY_NAMED);
NamedBody venus = new NamedBody(SolSystem4.VENUS_NAMED);
NamedBody vesta = new NamedBody(SolSystem4.VESTA_NAMED);
NamedBody pallas = new NamedBody(SolSystem4.PALLAS_NAMED);
NamedBody hygiea = new NamedBody(SolSystem4.HYGIEA_NAMED);
NamedBody ceres = new NamedBody(SolSystem4.CERES_NAMED);
// create some additional bodies
Body[] bodies = new Body[NUMBER_OF_BODIES];
@@ -56,9 +58,11 @@ public class Simulation6 {
Random random = new Random(2022);
for (int i = 0; i < bodies.length; i++) {
bodies[i] = new Body(Math.abs(random.nextGaussian()) * OVERALL_SYSTEM_MASS / bodies.length,
bodies[i] = new Body(
Math.abs(random.nextGaussian()) * OVERALL_SYSTEM_MASS / bodies.length,
new Vector3(0.2 * random.nextGaussian() * AU, 0.2 * random.nextGaussian() * AU, 0.2 * random.nextGaussian() * AU),
new Vector3(0 + random.nextGaussian() * 5e3, 0 + random.nextGaussian() * 5e3, 0 + random.nextGaussian() * 5e3));
new Vector3(0 + random.nextGaussian() * 5e3, 0 + random.nextGaussian() * 5e3, 0 + random.nextGaussian() * 5e3)
);
}
//TODO: implementation of this method according to 'Aufgabenblatt6.md'.