Struct LambertSolution 

pub struct LambertSolution {
    pub v_init_km_s: Vector3<f64>,
    pub v_final_km_s: Vector3<f64>,
    pub phi_rad: f64,
    pub input: LambertInput,
}

A solution to the Lambert problem.

Fields

v_init_km_s: Vector3<f64>

v_final_km_s: Vector3<f64>

phi_rad: f64

Turn angle ONLY computed with Godding method

input: LambertInput

Implementations

impl LambertSolution

pub fn v_inf_outgoing_km_s(&self) -> Vector3<f64>

Return the v infinity vector at departure, in km/s

pub fn v_inf_incoming_km_s(&self) -> Vector3<f64>

Return v infinity vector at arrival, in km/s

pub fn transfer_orbit(self) -> Orbit

Return the transfer orbit computed from setting the departure velocity to the initial state.

pub fn arrival_orbit(self) -> Orbit

Return the arrival orbit computed from setting the arrival velocity to the final state.

pub fn v_inf_outgoing_declination_deg(&self) -> f64

Return the declination of the departure v infinity (i.e. the outgoing asymptote velocity vector), in degrees

pub fn v_inf_outgoing_right_ascension_deg(&self) -> f64

Return the right ascention of the departure v infinity (i.e. the outgoing asymptote velocity vector), in degrees

pub fn c3_km2_s2(&self) -> f64

Returns the c3 computed as the departure v infinity norm squared

Trait Implementations

impl Clone for LambertSolution

fn clone(&self) -> LambertSolution

Returns a duplicate of the value.

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

Performs copy-assignment from source.

impl Debug for LambertSolution

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

Formats the value using the given formatter.

impl Copy for LambertSolution