Struct nyx_space::dynamics::thrustctrl::Ruggiero

pub struct Ruggiero { /* fields omitted */ }

Ruggiero defines the closed loop control law from IEPC 2011-102

Implementations

impl Ruggiero

The Ruggiero is a locally optimal control of a state for specific osculating elements. WARNING: Objectives must be in degrees!

pub fn new(objectives: Vec<Achieve>, initial: Orbit) -> Arc<Self>

Creates a new Ruggiero locally optimal control as an Arc Note: this returns an Arc so it can be plugged into the Spacecraft dynamics directly.

Trait Implementations

impl Clone for Ruggiero

fn clone(&self) -> Ruggiero

Returns a copy of the value.

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

Performs copy-assignment from source.

impl Copy for Ruggiero

impl Debug for Ruggiero

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

Formats the value using the given formatter.

impl ThrustControl for Ruggiero

fn achieved(&self, state: &SpacecraftState) -> Result<bool, NyxError>

Returns whether the control law has achieved all goals

fn direction(&self, sc: &SpacecraftState) -> Vector3<f64>

Returns a unit vector corresponding to the thrust direction in the inertial frame.

fn throttle(&self, sc: &SpacecraftState) -> f64

Returns a number between [0;1] corresponding to the engine throttle level. For example, 0 means coasting, i.e. no thrusting, and 1 means maximum thrusting.

fn next(&self, sc: &SpacecraftState) -> GuidanceMode

Update the state for the next iteration