Enum nyx_space::NyxError

pub enum NyxError {
    SingularStateTransitionMatrix,
    FuelExhausted(Box<Spacecraft>),
    ConditionNeverTriggered,
    UnsufficientTriggers(usize, usize),
    MaxIterReached(String),
    EventNotInEpochBraket(String, String),
    StateTransitionMatrixUnset,
    SensitivityNotUpdated,
    SingularKalmanGain,
    SingularCovarianceMatrix,
    CovarianceMatrixNotPsd,
    SingularJacobian,
    TargetsTooClose,
    LambertNotReasonablePhi,
    LambertMultiRevNotSupported,
    PartialsUndefined,
    StateParameterUnavailable,
    LoadingError(String),
    FileUnreadable(String),
    ObjectNotFound(String),
    NoInterpolationData(String),
    InvalidInterpolationData(String),
    NoStateData(String),
    DisjointFrameOrientations(String, String),
    NoThrusterAvail,
    CtrlNotAUnitVector(f64),
    CtrlThrottleRangeErr(f64),
    PolynomialOrderError(usize),
    NoObjectiveDefined,
    ExportError(String),
    NotHyperbolic(String),
    CorrectionIneffective(String),
    MonteCarlo(String),
    CCSDS(String),
    MultipleShootingTargeter(usize, Box<NyxError>),
    CustomError(String),
    TimeError(TimeErrors),
    Targeter(Box<TargetingError>),
    Trajectory(TrajError),
    MathDomain(String),
    GuidanceConfigError(String),
}

Nyx will (almost) never panic and functions which may fail will return an error.

Variants

SingularStateTransitionMatrix

STM is singular, propagation or smoothing cannot proceed

FuelExhausted(Box<Spacecraft>)

Fuel exhausted at the provided spacecraft state

ConditionNeverTriggered

Propagation event not triggered within the max propagation time

UnsufficientTriggers(usize, usize)

Propagation event not hit enough times (requested, found).

MaxIterReached(String)

Maximum iterations reached

EventNotInEpochBraket(String, String)

Event not found within the provided epochs

StateTransitionMatrixUnset

The operation was expecting the state to have an STM, but it isn’t present.

SensitivityNotUpdated

The sensitivity matrix must be updated prior to a filter measurement update

SingularKalmanGain

Kalman Gain could not be computed because HP_barH + R is singular

SingularCovarianceMatrix

Singular Covariance

CovarianceMatrixNotPsd

Covariance is not positive semi definite

SingularJacobian

Singular Jacobian

TargetsTooClose

Targets in Lambert solver too close: Δν ~=0 and A ~=0

LambertNotReasonablePhi

No reasonable phi found to connect both radii

LambertMultiRevNotSupported

Multi revolution Lambert not supported, use the Izzo algorithm for multi-rev transfers

PartialsUndefined

Partials for this dynamical model are not defined

StateParameterUnavailable

State parameter cannot be used in this function

LoadingError(String)

Could not load file

FileUnreadable(String)

Could not read file

ObjectNotFound(String)

Celestial object or spacecraft not found

NoInterpolationData(String)

No interpolation data

InvalidInterpolationData(String)

Invalid interpolation data

NoStateData(String)

No state data

DisjointFrameOrientations(String, String)

Cannot convert the state to another frame as the frames are disjoint

NoThrusterAvail

No thruster attached to spacecraft

CtrlNotAUnitVector(f64)

Control vector is not a unit vector

CtrlThrottleRangeErr(f64)

Throttle is not between 0.0 and 1.0

PolynomialOrderError(usize)

Happens when trying to modify a polynomial’s (error)-th error but the polynomial has less orders than that

NoObjectiveDefined

An objective based analysis or control was attempted, but no objective was defined

ExportError(String)

Error when exporting data

NotHyperbolic(String)

This computation requires the orbit to be hyperbolic

CorrectionIneffective(String)

Control variables to not decrease targeting error in differential corrector

MonteCarlo(String)

Monte Carlo error

CCSDS(String)

CCSDS error

MultipleShootingTargeter(usize, Box<NyxError>)

Multiple shooting failed with the provided error at the provided node computation

CustomError(String)

TimeError(TimeErrors)

Time related error

Targeter(Box<TargetingError>)

Targeting error

Trajectory(TrajError)

Trajectory error

MathDomain(String)

Math domain

GuidanceConfigError(String)

Guidance law config error

Trait Implementations

impl Clone for NyxError

fn clone(&self) -> NyxError

Returns a copy of the value.

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

Performs copy-assignment from source.

impl Debug for NyxError

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

Formats the value using the given formatter.

impl Display for NyxError

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

Formats the value using the given formatter.

impl Error for NyxError

fn source(&self) -> Option<&(dyn Error + 'static)>

The lower-level source of this error, if any.

fn description(&self) -> &str

👎Deprecated since 1.42.0: use the Display impl or to_string()

fn cause(&self) -> Option<&dyn Error>

👎Deprecated since 1.33.0: replaced by Error::source, which can support downcasting

fn provide<'a>(&'a self, demand: &mut Demand<'a>)

🔬This is a nightly-only experimental API. (error_generic_member_access)

Provides type based access to context intended for error reports.

impl From<Errors> for NyxError

fn from(e: TimeErrors) -> Self

Converts to this type from the input type.

impl From<NyxError> for ParsingError

fn from(error: NyxError) -> Self

Converts to this type from the input type.

impl From<TargetingError> for NyxError

fn from(e: TargetingError) -> Self

Converts to this type from the input type.

impl From<TrajError> for NyxError

fn from(e: TrajError) -> Self

Converts to this type from the input type.

impl PartialEq<NyxError> for NyxError

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

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

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

This method tests for !=. The default implementation is almost always sufficient, and should not be overridden without very good reason.

impl StructuralPartialEq for NyxError