Struct nyx_space::dynamics::solarpressure::SolarPressure

pub struct SolarPressure {
    pub phi: f64,
    pub e_loc: EclipseLocator,
}

Computation of solar radiation pressure is based on STK: http://help.agi.com/stk/index.htm#gator/eq-solar.htm .

Fields

phi: f64

solar flux at 1 AU, in W/m^2

e_loc: EclipseLocator

Implementations

impl SolarPressure

pub fn default_raw(shadow_bodies: Vec<Frame>, cosm: Arc<Cosm>) -> Self

Will set the solar flux at 1 AU to: Phi = 1367.0

pub fn default(shadow_body: Frame, cosm: Arc<Cosm>) -> Arc<Self>

Accounts for the shadowing of only one body and will set the solar flux at 1 AU to: Phi = 1367.0

pub fn with_flux( flux_w_m2: f64, shadow_bodies: Vec<Frame>, cosm: Arc<Cosm> ) -> Arc<Self>

Must provide the flux in W/m^2

Trait Implementations

impl Clone for SolarPressure

fn clone(&self) -> SolarPressure

Returns a copy of the value.

fn clone_from(&mut self, source: &Self)

Performs copy-assignment from source.

impl Display for SolarPressure

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

Formats the value using the given formatter.

impl<X: SpacecraftExt> ForceModel<X> for SolarPressure

fn eom(&self, ctx: &BaseSpacecraft<X>) -> Result<Vector3<f64>, NyxError>

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

fn dual_eom( &self, ctx: &BaseSpacecraft<X> ) -> Result<(Vector3<f64>, Matrix3<f64>), NyxError>

Force models must implement their partials, although those will only be called if the propagation requires the computation of the STM. The osc_ctx is the osculating context, i.e. it changes for each sub-step of the integrator.