sidereon_core/astro/
state.rs

1use nalgebra::Vector3;
2
3#[derive(Debug, Clone, Copy, PartialEq)]
4pub struct CartesianState {
5    pub epoch_tdb_seconds: f64,
6    pub position_km: Vector3<f64>,
7    pub velocity_km_s: Vector3<f64>,
8}
9
10impl CartesianState {
11    pub fn new(epoch_tdb_seconds: f64, position: [f64; 3], velocity: [f64; 3]) -> Self {
12        Self {
13            epoch_tdb_seconds,
14            position_km: Vector3::from_column_slice(&position),
15            velocity_km_s: Vector3::from_column_slice(&velocity),
16        }
17    }
18
19    pub fn position_array(&self) -> [f64; 3] {
20        [self.position_km.x, self.position_km.y, self.position_km.z]
21    }
22
23    pub fn velocity_array(&self) -> [f64; 3] {
24        [
25            self.velocity_km_s.x,
26            self.velocity_km_s.y,
27            self.velocity_km_s.z,
28        ]
29    }
30}
31
32#[derive(Debug, Clone, Copy)]
33pub struct StateDerivative {
34    pub dpos_km_s: Vector3<f64>,
35    pub dvel_km_s2: Vector3<f64>,
36}
37
38impl StateDerivative {
39    pub fn new(dpos: Vector3<f64>, dvel: Vector3<f64>) -> Self {
40        Self {
41            dpos_km_s: dpos,
42            dvel_km_s2: dvel,
43        }
44    }
45}
sidereon_core/astro/state.rs

sidereon_core/astro/
state.rs
