Compare commits
5 Commits
5197362280
...
cc3844f920
Author | SHA1 | Date |
---|---|---|
ktyl | cc3844f920 | |
ktyl | 694b2b576c | |
ktyl | 70c4cd8a92 | |
ktyl | 5ad70b3f9c | |
ktyl | bed71f2c4c |
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@ -1,7 +1,7 @@
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[gd_scene load_steps=3 format=2]
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[gd_scene load_steps=3 format=2]
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[ext_resource path="res://scenes/OrbitCamera.tscn" type="PackedScene" id=3]
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[ext_resource path="res://scenes/OrbitCamera.tscn" type="PackedScene" id=3]
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||||||
[ext_resource path="res://scenes/orbits/OrbitSystem.tscn" type="PackedScene" id=4]
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[ext_resource path="res://scenes/orbits/Barycenter.tscn" type="PackedScene" id=4]
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[node name="Main" type="Node2D"]
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[node name="Main" type="Node2D"]
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@ -10,9 +10,8 @@ transform = Transform( 0.515898, 0.606099, -0.605386, -0.393123, 0.795389, 0.461
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[node name="OrbitCamera" parent="." instance=ExtResource( 3 )]
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[node name="OrbitCamera" parent="." instance=ExtResource( 3 )]
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[node name="Orbit System" parent="." instance=ExtResource( 4 )]
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[node name="Barycenter" parent="." instance=ExtResource( 4 )]
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transform = Transform( 0.856869, 0.3292, -0.396741, 0.0949996, 0.655565, 0.749139, 0.506706, -0.679604, 0.53046, -0.599122, 0, 0 )
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transform = Transform( 0.856869, 0.3292, -0.396741, 0.0949996, 0.655565, 0.749139, 0.506706, -0.679604, 0.53046, -0.599122, 0, 0 )
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SemiMajorAxis = 6.166
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SemiMajorAxis = 6.166
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Eccentricity = 0.239
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Eccentricity = 0.239
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Period = 1.0
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_speed = 0.877
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_speed = 0.877
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@ -0,0 +1,18 @@
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[gd_scene load_steps=3 format=2]
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[ext_resource path="res://scripts/orbits/Barycenter.cs" type="Script" id=1]
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[ext_resource path="res://scenes/orbits/Planet.tscn" type="PackedScene" id=2]
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[node name="Barycenter" type="Spatial"]
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script = ExtResource( 1 )
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SemiMajorAxis = 7.0
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Eccentricity = 0.752
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_pointMassPaths = [ NodePath("Planet A"), NodePath("Planet B") ]
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_speed = 1.0
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[node name="Planet A" parent="." instance=ExtResource( 2 )]
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transform = Transform( 0.999977, 0.00603502, 0.00319089, -0.00604282, 0.999979, 0.0024369, -0.00317609, -0.00245615, 0.999992, -2.55711, 0, -4.25519 )
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[node name="Planet B" parent="." instance=ExtResource( 2 )]
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transform = Transform( 0.5, 0, 0, 0, 0.5, 0, 0, 0, 0.5, -11.9998, 0, 1.25565 )
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Mass = 0.125
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@ -1,22 +0,0 @@
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[gd_scene load_steps=3 format=2]
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[ext_resource path="res://scripts/orbits/OrbitSystem.cs" type="Script" id=1]
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[ext_resource path="res://scenes/orbits/Planet.tscn" type="PackedScene" id=2]
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[node name="Orbit System" type="Spatial"]
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script = ExtResource( 1 )
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SemiMajorAxis = 6.881
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Eccentricity = 0.399
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Period = 10.0
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_a = NodePath("Planet A")
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_b = NodePath("Planet B")
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_barycenter = NodePath("Barycenter")
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[node name="Barycenter" type="Spatial" parent="."]
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[node name="Planet A" parent="." instance=ExtResource( 2 )]
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transform = Transform( 0.999977, 0.00603502, 0.00319089, -0.00604282, 0.999979, 0.0024369, -0.00317609, -0.00245615, 0.999992, 0, 0, 0 )
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[node name="Planet B" parent="." instance=ExtResource( 2 )]
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transform = Transform( 0.5, 0, 0, 0, 0.5, 0, 0, 0, 0.5, -8.44634, 0, -3.53339 )
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Mass = 0.125
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@ -1,13 +1,13 @@
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using Godot;
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using Godot;
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using System;
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using System;
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using System.Collections.Generic;
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using Vim.Math3d;
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using Vim.Math3d;
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[Tool]
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[Tool]
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public class OrbitSystem : Node, IMassive, ILocation
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public class Barycenter : Node, IPointMass
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{
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{
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[Export] private NodePath _a;
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[Export]
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[Export] private NodePath _b;
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private NodePath[] _pointMassPaths;
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[Export] private NodePath _barycenter;
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private double _semiMajorAxis;
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private double _semiMajorAxis;
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[Export]
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[Export]
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||||||
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@ -40,79 +40,19 @@ public class OrbitSystem : Node, IMassive, ILocation
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}
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}
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}
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}
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#region Point Masses
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public double Mass
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private IPointMass Primary
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{
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{
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get
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get
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{
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{
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if (_pointMasses[0] == null)
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double mass = 0;
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foreach (var orbiter in Orbiters)
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{
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{
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InitPointMasses();
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mass += orbiter.PointMass.Mass;
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}
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}
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return _pointMasses[0];
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return mass;
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}
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}
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private IPointMass Secondary
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{
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get
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{
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if (_pointMasses[1] == null)
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{
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InitPointMasses();
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}
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return _pointMasses[1];
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}
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}
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private readonly IPointMass[] _pointMasses = new IPointMass[2];
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private void InitPointMasses()
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{
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var a = GetNode<IPointMass>(_a);
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var b = GetNode<IPointMass>(_b);
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if (a.Mass > b.Mass)
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{
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_pointMasses[0] = a;
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_pointMasses[1] = b;
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}
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else
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{
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_pointMasses[0] = b;
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_pointMasses[1] = a;
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}
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}
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#endregion
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public float Mass => Primary.Mass + Secondary.Mass;
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public DVector3 Position
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{
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get => Barycenter;
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set => Barycenter = value;
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}
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public DVector3 Barycenter
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{
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get
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{
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var p0 = Primary.Position;
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var p1 = Secondary.Position;
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return p0.Lerp(p1, .5f);
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}
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// TODO - make setting the berycenter do something sensible?
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set => _ = value;
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}
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private Orbit _orbit = null;
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private Orbit Orbit
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{
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get
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{
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if (_orbit == null)
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{
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_orbit = new Orbit();
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}
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return _orbit;
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}
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}
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}
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}
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public DVector3 Position { get; set; }
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private ImmediateGeometry _orbitGeometry = null;
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private ImmediateGeometry _orbitGeometry = null;
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public ImmediateGeometry OrbitGeometry
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public ImmediateGeometry OrbitGeometry
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@ -132,6 +72,50 @@ public class OrbitSystem : Node, IMassive, ILocation
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}
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}
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}
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}
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private struct Orbiter
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{
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public IPointMass PointMass { get; set; }
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public IOrbit Orbit { get; set; }
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}
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private Orbiter[] _orbiters = null;
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private Orbiter[] Orbiters
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{
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get
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||||||
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{
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if (_orbiters == null)
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||||||
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{
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var length = _pointMassPaths.Length;
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_orbiters = new Orbiter[length];
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for (int i = 0; i < length; i++)
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{
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var pointMass = GetNode<IPointMass>(_pointMassPaths[i]);
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var orbit = new Orbit(this, pointMass);
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var orbiter = new Orbiter
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{
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PointMass = pointMass,
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Orbit = orbit
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};
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_orbiters[i] = orbiter;
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}
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}
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return _orbiters;
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}
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||||||
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}
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||||||
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private IOrbit[] _orbits;
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private IOrbit[] Orbits
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{
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||||||
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get
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||||||
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{
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||||||
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if (_orbits == null)
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||||||
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{
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||||||
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||||||
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}
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||||||
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return _orbits;
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}
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}
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private float _time = 0;
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private float _time = 0;
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[Export]
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[Export]
|
||||||
|
@ -145,9 +129,15 @@ public class OrbitSystem : Node, IMassive, ILocation
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private void InvalidateGeometry()
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private void InvalidateGeometry()
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{
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{
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Orbit.Ellipse = new Ellipse(SemiMajorAxis, Eccentricity);
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for (int i = 0; i < Orbiters.Length; i++)
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Orbit.Draw(OrbitGeometry);
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{
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var orbiter = Orbiters[i];
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var orbit = orbiter.Orbit;
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orbit.Ellipse = new Ellipse(SemiMajorAxis, Eccentricity);
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orbit.Draw(OrbitGeometry);
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Secondary.Position = Orbit.GetPosition(_time);
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var t = _time + i * Math.PI;
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orbiter.PointMass.Position = orbit.GetPosition(t);
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}
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}
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}
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}
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}
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@ -3,5 +3,5 @@ using System;
|
||||||
|
|
||||||
public interface IMassive
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public interface IMassive
|
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{
|
{
|
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float Mass { get; }
|
double Mass { get; }
|
||||||
}
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}
|
||||||
|
|
|
@ -0,0 +1,4 @@
|
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public static class IMassiveExtensions
|
||||||
|
{
|
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public static double U(this IMassive m) => Kepler.U(m.Mass);
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}
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@ -0,0 +1,7 @@
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using Vim.Math3d;
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public interface IOrbit
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{
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DVector3 GetPosition(double t);
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IEllipse Ellipse { get; set; }
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}
|
|
@ -0,0 +1,29 @@
|
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using Godot;
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|
|
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public static class IOrbitExtensions
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||||||
|
{
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public static void Draw(this IOrbit orbit, ImmediateGeometry geo)
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|
{
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geo.Clear();
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geo.Begin(Mesh.PrimitiveType.LineLoop);
|
||||||
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geo.SetColor(new Color(1, 0, 0));
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|
|
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int steps = 100;
|
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var ellipse = orbit.Ellipse;
|
||||||
|
|
||||||
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for (int i = 0; i < steps; i++)
|
||||||
|
{
|
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|
float t = i / (float)steps;
|
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float a = t * Mathf.Tau;
|
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|
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var v2 = ellipse.Foci[0] + ellipse.GetPosition(a);
|
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|
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geo.AddVertex(new Godot.Vector3
|
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|
{
|
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x = (float)v2.X,
|
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z = (float)v2.Y
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|
});
|
||||||
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}
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||||||
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geo.End();
|
||||||
|
}
|
||||||
|
}
|
|
@ -2,56 +2,42 @@ using Godot;
|
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using System;
|
using System;
|
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using Vim.Math3d;
|
using Vim.Math3d;
|
||||||
|
|
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public class Orbit
|
public class Orbit : IOrbit
|
||||||
{
|
{
|
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// The position of the primary body relative to the ellipse - the
|
public IEllipse Ellipse { get; set; }
|
||||||
// orbit itself is presented as being centred on the primary, but
|
|
||||||
// all our math is elliptical.
|
|
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private DVector2 PrimaryPosition => Ellipse.Focus0;
|
|
||||||
|
|
||||||
public Ellipse Ellipse { get; set; }
|
private readonly IMassive _massive;
|
||||||
|
private readonly ILocation _satellite;
|
||||||
|
|
||||||
public DVector3 GetPosition(float t)
|
/// <summary>
|
||||||
|
/// An orbit is treated as one stationary body at one focus of the orbit's ellipse.
|
||||||
|
/// The satellite is treated as a massless point.
|
||||||
|
/// </summary>
|
||||||
|
/// <param name="massive">Mass of the object being orbited</param>
|
||||||
|
/// <param name="satellite">The orbiting body</param>
|
||||||
|
public Orbit(IMassive massive, ILocation satellite)
|
||||||
{
|
{
|
||||||
// TODO: determine period from mass of orbiting bodies
|
// TODO: determine ellipse better
|
||||||
var P = 10f;
|
// semi-major axis is distance of satellite from origin
|
||||||
|
var a = satellite.Position.Magnitude();
|
||||||
|
var e = 0.8f;
|
||||||
|
this.Ellipse = new Ellipse(a, e);
|
||||||
|
|
||||||
|
_massive = massive;
|
||||||
|
_satellite = satellite;
|
||||||
|
}
|
||||||
|
|
||||||
|
public DVector3 GetPosition(double t)
|
||||||
|
{
|
||||||
var a = Ellipse.a;
|
var a = Ellipse.a;
|
||||||
var e = Ellipse.e;
|
var e = Ellipse.e;
|
||||||
|
|
||||||
|
var P = Kepler.GetPeriod(a, _massive.U());
|
||||||
|
|
||||||
var M = Kepler.GetMeanAnomaly(t, P);
|
var M = Kepler.GetMeanAnomaly(t, P);
|
||||||
var E = Kepler.GetEccentricAnomaly(e, M) + Math.PI;
|
var E = Kepler.GetEccentricAnomaly(e, M) + Math.PI;
|
||||||
|
|
||||||
var p = Kepler.GetEccentricPosition2D(e, a, t);
|
var p = Kepler.GetEccentricPosition2D(e, a, t);
|
||||||
return new DVector3(p.X, 0, p.Y);
|
return new DVector3(p.X, 0, p.Y);
|
||||||
}
|
}
|
||||||
|
|
||||||
public void Draw(ImmediateGeometry geo)
|
|
||||||
{
|
|
||||||
geo.Clear();
|
|
||||||
geo.Begin(Mesh.PrimitiveType.LineLoop);
|
|
||||||
DrawEllipse(geo);
|
|
||||||
geo.End();
|
|
||||||
}
|
|
||||||
|
|
||||||
private void DrawEllipse(ImmediateGeometry geo)
|
|
||||||
{
|
|
||||||
geo.SetColor(new Color(1, 0, 0));
|
|
||||||
|
|
||||||
int steps = 100;
|
|
||||||
|
|
||||||
for (int i = 0; i < steps; i++)
|
|
||||||
{
|
|
||||||
float t = i / (float)steps;
|
|
||||||
float a = t * Mathf.Tau;
|
|
||||||
|
|
||||||
var v2 = Ellipse.Focus0 + Ellipse.GetPosition(a);
|
|
||||||
|
|
||||||
geo.AddVertex(new Godot.Vector3
|
|
||||||
{
|
|
||||||
x = (float)v2.X,
|
|
||||||
z = (float)v2.Y
|
|
||||||
});
|
|
||||||
}
|
|
||||||
}
|
|
||||||
}
|
}
|
||||||
|
|
|
@ -6,7 +6,7 @@ using Vim.Math3d;
|
||||||
public class Planet : Spatial, IPointMass
|
public class Planet : Spatial, IPointMass
|
||||||
{
|
{
|
||||||
[Export]
|
[Export]
|
||||||
public float Mass { get; set; }
|
public double Mass { get; set; }
|
||||||
|
|
||||||
private DVector3? _position;
|
private DVector3? _position;
|
||||||
public DVector3 Position
|
public DVector3 Position
|
||||||
|
|
|
@ -2,7 +2,7 @@ using Godot;
|
||||||
using System;
|
using System;
|
||||||
using Vim.Math3d;
|
using Vim.Math3d;
|
||||||
|
|
||||||
public struct Ellipse
|
public struct Ellipse : IEllipse
|
||||||
{
|
{
|
||||||
public Ellipse(double a = 1, double e = 0)
|
public Ellipse(double a = 1, double e = 0)
|
||||||
{
|
{
|
||||||
|
@ -12,6 +12,16 @@ public struct Ellipse
|
||||||
// TODO: this is an immutable struct, so initialise everything else
|
// TODO: this is an immutable struct, so initialise everything else
|
||||||
// in the constructor to avoid recalculating properties whenever
|
// in the constructor to avoid recalculating properties whenever
|
||||||
// they are accessed
|
// they are accessed
|
||||||
|
|
||||||
|
Apisides = new Apisides(a, e);
|
||||||
|
b = Math.Sqrt(Apisides.max * Apisides.min);
|
||||||
|
|
||||||
|
var d = Math.Sqrt(a * a - b * b);
|
||||||
|
Foci = new DVector2[]
|
||||||
|
{
|
||||||
|
new DVector2(-d, 0),
|
||||||
|
new DVector2(d, 0)
|
||||||
|
};
|
||||||
}
|
}
|
||||||
|
|
||||||
/// <summary>
|
/// <summary>
|
||||||
|
@ -29,8 +39,7 @@ public struct Ellipse
|
||||||
/// <summary>
|
/// <summary>
|
||||||
/// Semi-minor axis
|
/// Semi-minor axis
|
||||||
/// </summary>
|
/// </summary>
|
||||||
public double b => SemiMinorAxis;
|
public double b { get; }
|
||||||
public double SemiMinorAxis => Math.Sqrt(Apisides.max * Apisides.min);
|
|
||||||
|
|
||||||
/// <summary>
|
/// <summary>
|
||||||
/// Get a position on the auxiliary circle
|
/// Get a position on the auxiliary circle
|
||||||
|
@ -40,13 +49,10 @@ public struct Ellipse
|
||||||
public DVector2 GetAuxiliaryPosition2D(double t = 0) =>
|
public DVector2 GetAuxiliaryPosition2D(double t = 0) =>
|
||||||
new DVector2(Math.Cos(t), Math.Sin(t)) * a;
|
new DVector2(Math.Cos(t), Math.Sin(t)) * a;
|
||||||
|
|
||||||
private Apisides Apisides => new Apisides(a, e);
|
private Apisides Apisides { get; }
|
||||||
|
|
||||||
public DVector2 GetPosition(double t) =>
|
public DVector2[] Foci { get; }
|
||||||
new DVector2(Math.Cos(t) * a, Math.Sin(t) * b);
|
|
||||||
|
|
||||||
public DVector2 Focus0 => new DVector2(-GetFocusDistance(), 0);
|
|
||||||
public DVector2 Focus1 => new DVector2(GetFocusDistance(), 0);
|
|
||||||
private double GetFocusDistance() => Math.Sqrt(a * a - b * b);
|
private double GetFocusDistance() => Math.Sqrt(a * a - b * b);
|
||||||
}
|
}
|
||||||
|
|
||||||
|
|
|
@ -0,0 +1,20 @@
|
||||||
|
using Godot;
|
||||||
|
using System;
|
||||||
|
using Vim.Math3d;
|
||||||
|
|
||||||
|
public interface IEllipse
|
||||||
|
{
|
||||||
|
/// <summary>
|
||||||
|
/// Semi-major axis
|
||||||
|
/// </summary>
|
||||||
|
double a { get; }
|
||||||
|
double b { get; }
|
||||||
|
/// <summary>
|
||||||
|
/// Eccentricity
|
||||||
|
/// </summary>
|
||||||
|
double e { get; }
|
||||||
|
/// <summary>
|
||||||
|
/// Positions of the two foci of the ellipse
|
||||||
|
/// </summary>
|
||||||
|
DVector2[] Foci { get; }
|
||||||
|
}
|
|
@ -0,0 +1,8 @@
|
||||||
|
using Vim.Math3d;
|
||||||
|
using System;
|
||||||
|
|
||||||
|
public static class IEllipseExtensions
|
||||||
|
{
|
||||||
|
public static DVector2 GetPosition(this IEllipse e, double t) =>
|
||||||
|
new DVector2(Math.Cos(t) * e.a, Math.Sin(t) * e.b);
|
||||||
|
}
|
Loading…
Reference in New Issue