Struct PointMasses

pub struct PointMasses {
    pub celestial_objects: Vec<i32>,
    pub correction: Option<Aberration>,
}

PointMasses model

Fields

celestial_objects: Vec<i32>

correction: Option<Aberration>

Light-time correction computation if extra point masses are needed

Implementations

impl PointMasses

pub fn new(celestial_objects: Vec<i32>) -> Arc<Self>

Initializes the point masses gravities with the provided list of bodies

pub fn with_correction( celestial_objects: Vec<i32>, correction: Aberration, ) -> Self

Initializes the point masses gravities with the provided list of bodies, and accounting for some light time correction

Trait Implementations

impl AccelModel for PointMasses

fn eom( &self, osc: &Orbit, almanac: Arc<Almanac>, ) -> Result<Vector3<f64>, DynamicsError>

Defines the equations of motion for this force model from the provided osculating state in the integration frame.

fn dual_eom( &self, osc: &Orbit, almanac: Arc<Almanac>, ) -> Result<(Vector3<f64>, Matrix3<f64>), DynamicsError>

Acceleration models must implement their partials, although those will only be called if the propagation requires the computation of the STM.

impl Display for PointMasses

fn fmt(&self, f: &mut Formatter<'_>) -> Result

Formats the value using the given formatter.