use crate::astro::constants::{J2_EARTH, MU_EARTH, RE_EARTH};
use crate::astro::error::PropagationError;
use crate::astro::forces::r#trait::ForceModel;
use crate::astro::propagator::api::PropagationContext;
use crate::astro::state::CartesianState;
use nalgebra::Vector3;
pub struct J2Gravity {
pub mu: f64,
pub re: f64,
pub j2: f64,
}
impl Default for J2Gravity {
fn default() -> Self {
Self {
mu: MU_EARTH,
re: RE_EARTH,
j2: J2_EARTH,
}
}
}
impl ForceModel for J2Gravity {
fn acceleration(
&self,
state: &CartesianState,
_ctx: &PropagationContext,
) -> Result<Vector3<f64>, PropagationError> {
let r_mag2 = state.position_km.norm_squared();
if r_mag2 == 0.0 {
return Err(PropagationError::NumericalFailure(
"Zero position magnitude".to_string(),
));
}
let r_mag = r_mag2.sqrt();
let f = 1.5 * self.j2 * (self.mu / r_mag2) * (self.re / r_mag).powi(2);
let z_r2 = (state.position_km.z * state.position_km.z) / r_mag2;
Ok(Vector3::new(
f * (state.position_km.x / r_mag) * (5.0 * z_r2 - 1.0),
f * (state.position_km.y / r_mag) * (5.0 * z_r2 - 1.0),
f * (state.position_km.z / r_mag) * (5.0 * z_r2 - 3.0),
))
}
}
#[cfg(test)]
mod tests {
use super::*;
use crate::astro::propagator::api::PropagationContext;
use crate::astro::state::CartesianState;
#[test]
fn acceleration_matches_orbis_force_wrapper_bits() {
let state = CartesianState::new(0.0, [7000.0, -1210.0, 1300.0], [0.0, 0.0, 0.0]);
let acceleration = J2Gravity::default()
.acceleration(&state, &PropagationContext::default())
.unwrap();
assert_eq!(acceleration.x.to_bits(), 13_754_131_348_549_160_135);
assert_eq!(acceleration.y.to_bits(), 4_519_025_615_523_880_849);
assert_eq!(acceleration.z.to_bits(), 13_750_824_904_549_515_386);
}
}