Struct nyx_space::dynamics::spacecraft::Spacecraft

pub struct Spacecraft<'a, T: ThrustControl> {
    pub celestial: CelestialDynamics<'a>,
    pub force_models: Vec<Box<dyn ForceModel + 'a>>,
    pub prop: Option<Propulsion<T>>,
    pub dry_mass: f64,
    pub fuel_mass: f64,
    // some fields omitted
}

Fields

celestial: CelestialDynamics<'a>

force_models: Vec<Box<dyn ForceModel + 'a>>

prop: Option<Propulsion<T>>

dry_mass: f64

in kg

fuel_mass: f64

in kg

Methods

impl<'a, T: ThrustControl> Spacecraft<'a, T>

pub fn with_prop(
    celestial: CelestialDynamics<'a>,
    prop: Propulsion<T>,
    dry_mass: f64,
    fuel_mass: f64
) -> Self

Initialize a Spacecraft with a set of celestial dynamics and a propulsion subsystem.

pub fn new(celestial: CelestialDynamics<'a>, dry_mass: f64) -> Self

Initialize a Spacecraft with a set of celestial dynamics and with SRP enabled.

pub fn add_model(&mut self, force_model: Box<dyn ForceModel + 'a>)

Trait Implementations

impl<'a, T: ThrustControl> Dynamics for Spacecraft<'a, T>

type StateSize = U7

Defines the state size for these dynamics. It must be imported from nalgebra.

type StateType = SpacecraftState

Defines the type which will be published on the propagator channel

fn time(&self) -> f64

Returns the time of the current state

fn state(&self) -> Self::StateType

Returns the state of the dynamics

fn state_vector(&self) -> VectorN<f64, Self::StateSize>

Returns the current state of the dynamics as a vector so it can be integrated.

fn set_state(&mut self, new_t: f64, new_state: &VectorN<f64, Self::StateSize>)

Updates the internal state of the dynamics.

fn eom(
    &self,
    t: f64,
    state: &VectorN<f64, Self::StateSize>
) -> VectorN<f64, Self::StateSize>

Defines the equations of motion for these dynamics, or a combination of provided dynamics.