Enum AeroError 

#[non_exhaustive]
pub enum AeroError {
    Domain {
        what: &'static str,
        value: f64,
    },
    Mach {
        mach: f64,
        limit: f64,
        model: &'static str,
    },
    Unsupported(String),
    Layout(String),
    InComponent {
        id: String,
        source: Box<AeroError>,
    },
    DragModel {
        source: Box<AeroError>,
    },
    Design(DesignError),
    Csv {
        line: usize,
        message: String,
    },
    Table(CoreError),
}

An error from the aerodynamic models: an input outside the models’ domain, a design they can’t describe, or an error from the design itself.

Variants (Non-exhaustive)

Non-exhaustive enums could have additional variants added in future. Therefore, when matching against variants of non-exhaustive enums, an extra wildcard arm must be added to account for any future variants.

Domain

An input outside its domain, such as a negative span or a non-finite angle.

Fields

what: &'static str

What the value is.

value: f64

The offending value.

Mach

A Mach number past the range of the model asked: 0 ≤ M < 5 for the normal force (crate::model::NORMAL_FORCE_MACH_LIMIT) and the drag buildup (crate::drag::BUILDUP_MACH_LIMIT); an override table takes any Mach number.

Fields

mach: f64

The Mach number.

limit: f64

The top of the model’s range, which it doesn’t reach.

model: &'static str

The model that refused it, such as “the drag buildup”.

Unsupported(String)

A part the models have no cited method for, such as tube fins.

Layout(String)

A layout that doesn’t hold together for the aerodynamic models, such as a fin set without the radius of its body tube.

InComponent

An error in one component, with its id.

Fields

id: String

The component’s id.

source: Box<AeroError>

The error.

DragModel

An error from a drag model of a program’s own (crate::custom::DragModel), as it gave it: its own refusal, or one of hpr’s it passed on.

Fields

source: Box<AeroError>

The error.

Design(DesignError)

An error from the design model, such as a profile whose volume integral fails.

Csv

CSV text that doesn’t read as a table, with its 1-based line (0 when the text has no rows).

Fields

line: usize

The line, counting from 1.

message: String

What is wrong.

Table(CoreError)

A table that doesn’t hold together, such as Mach numbers that don’t increase.

Trait Implementations

impl Clone for AeroError

fn clone(&self) -> AeroError

Returns a duplicate of the value.

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

Performs copy-assignment from source.

impl Debug for AeroError

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

Formats the value using the given formatter.

impl Display for AeroError

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

Formats the value using the given formatter.

impl Error for AeroError

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

Returns 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, request: &mut Request<'a>)

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

Provides type-based access to context intended for error reports.

impl From<CoreError> for AeroError

fn from(source: CoreError) -> Self

Converts to this type from the input type.

impl From<DesignError> for AeroError

fn from(source: DesignError) -> Self

Converts to this type from the input type.

impl PartialEq for AeroError

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

Tests for self and other values to be equal, and is used by ==.

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

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

impl StructuralPartialEq for AeroError