Struct nyx_space::dynamics::thrustctrl::Ruggiero

pub struct Ruggiero { /* fields omitted */ }

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

Methods

impl Ruggiero

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

pub fn new(objectives: Vec<Achieve>, initial: State<Geoid>) -> Self

pub fn achieved(&self, state: &State<Geoid>) -> bool

Returns whether the control law has achieved all goals

Trait Implementations

impl ThrustControl for Ruggiero

fn direction(&self, dt: Epoch, state: &Vector6<f64>) -> Vector3<f64>

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

fn throttle(&self, dt: Epoch, state: &Vector6<f64>) -> 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(&mut self, dt: Epoch, state: &Vector6<f64>)

Update the state for the next iteration

impl Clone for Ruggiero

fn clone(&self) -> Ruggiero

Returns a copy of the value.

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

Performs copy-assignment from source.

impl Debug for Ruggiero

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

Formats the value using the given formatter.