Enum nyx_space::dynamics::spacecraft::GuidanceMode

pub enum GuidanceMode {
    Coast,
    Thrust,
    Inhibit,
    Custom(u8),
}

Variants

Coast

Guidance is turned off and Guidance Law may switch mode to Thrust for next call

Thrust

Guidance is turned on and Guidance Law may switch mode to Coast for next call

Inhibit

Guidance is turned off and Guidance Law may not change its mode (will need to be done externally to the guidance law).

Custom(u8)

Trait Implementations

impl Clone for GuidanceMode

fn clone(&self) -> GuidanceMode

Returns a copy of the value.

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

Performs copy-assignment from source.

impl Debug for GuidanceMode

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

Formats the value using the given formatter.

impl Default for GuidanceMode

fn default() -> Self

Returns the “default value” for a type.

impl GuidanceLaw<GuidanceMode> for FiniteBurns

fn direction(&self, osc: &Spacecraft) -> Vector3<f64>

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

fn throttle(&self, osc: &Spacecraft) -> 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: &mut Spacecraft)

Updates the state of the spacecraft for the next maneuver, e.g. prepares the controller for the next maneuver

fn achieved(&self, _osc_state: &BaseSpacecraft<X>) -> Result<bool, NyxError>

Returns whether this thrust control has been achieved, if it has an objective

impl GuidanceLaw<GuidanceMode> for Mnvr

fn direction(&self, osc: &Spacecraft) -> Vector3<f64>

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

fn throttle(&self, osc: &Spacecraft) -> 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: &mut Spacecraft)

Updates the state of the spacecraft for the next maneuver, e.g. prepares the controller for the next maneuver

fn achieved(&self, _osc_state: &BaseSpacecraft<X>) -> Result<bool, NyxError>

Returns whether this thrust control has been achieved, if it has an objective

impl GuidanceLaw<GuidanceMode> for Ruggiero

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

Returns whether the guidance law has achieved all goals

fn next(&self, sc: &mut Spacecraft)

Update the state for the next iteration

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

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

fn throttle(&self, sc: &Spacecraft) -> 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.

impl PartialEq<GuidanceMode> for GuidanceMode

fn eq(&self, other: &GuidanceMode) -> bool

This method tests for self and other values to be equal, and is used by ==.

fn ne(&self, other: &GuidanceMode) -> bool

This method tests for !=.

impl Copy for GuidanceMode

impl SpacecraftExt for GuidanceMode

impl StructuralPartialEq for GuidanceMode