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Advanced orbit calculations

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This commit is contained in:
Verox001 2025-05-04 22:55:55 +02:00
parent 0618b81763
commit 5cd61b6086
2 changed files with 5 additions and 16 deletions
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7
simulator/src/main.rs
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@ -316,10 +316,11 @@ impl<'a> State<'a> {
let instances = {
let sim = simulator.read().unwrap();
let sun_pos = sim.bodies[0].position;
sim.bodies.iter().enumerate().map(|(i, b)| RenderInstance {
position: cgmath::Vector3::new(
(b.position[0] / 1.496e11) as f32,
(b.position[1] / 1.496e11) as f32,
((b.position[0] - sun_pos[0]) / 1.496e11) as f32,
((b.position[1] - sun_pos[1]) / 1.496e11) as f32,
0.0,
),
rotation: cgmath::Quaternion::from_angle_z(cgmath::Deg(0.0)),
@ -474,7 +475,7 @@ impl<'a> State<'a> {
format: surface_format,
width: size.width,
height: size.height,
present_mode: PresentMode::AutoNoVsync,
present_mode: PresentMode::AutoVsync,
alpha_mode: capabilities.alpha_modes[0],
view_formats: vec![],
desired_maximum_frame_latency: 2,

12
solar_engine/src/simulator.rs
View File

@ -88,7 +88,6 @@ impl Simulator {
.collect()
}
// RK4 Stufen
let k1_pos = original_states.iter().map(|s| s.velocity).collect::<Vec<_>>();
let k1_vel = compute_accelerations(&original_states, &masses);
@ -130,10 +129,8 @@ impl Simulator {
let k4_pos = temp_states.iter().map(|s| s.velocity).collect::<Vec<_>>();
let k4_vel = compute_accelerations(&temp_states, &masses);
// Finale Updates
for i in 0..n {
let body = &mut self.bodies[i];
let old_position = body.position;
body.position[0] += (dt / 6.0)
* (k1_pos[i][0] + 2.0 * k2_pos[i][0] + 2.0 * k3_pos[i][0] + k4_pos[i][0]);
@ -144,15 +141,6 @@ impl Simulator {
* (k1_vel[i][0] + 2.0 * k2_vel[i][0] + 2.0 * k3_vel[i][0] + k4_vel[i][0]);
body.velocity[1] += (dt / 6.0)
* (k1_vel[i][1] + 2.0 * k2_vel[i][1] + 2.0 * k3_vel[i][1] + k4_vel[i][1]);
// Bewegung loggen
let dx = body.position[0] - old_position[0];
let dy = body.position[1] - old_position[1];
let movement = (dx * dx + dy * dy).sqrt();
if i == 1 {
println!("Earth moved {:.6} meters", movement);
}
}
self.time += dt;