Enum OrbitType 

pub enum OrbitType {
    EllipticalInclined,
    EllipticalEquatorial,
    CircularInclined,
    CircularEquatorial,
}

Geometric classification of a two-body orbit, which determines which of the classical elements are defined and which auxiliary angle resolves the degenerate ones.

Variants

EllipticalInclined

Eccentric and inclined: all six classical elements are defined.

EllipticalEquatorial

Eccentric but equatorial: the ascending node is undefined; the longitude of perigee (ClassicalElements::lonper) replaces it.

CircularInclined

Circular but inclined: the argument of perigee is undefined; the argument of latitude (ClassicalElements::arglat) replaces it.

CircularEquatorial

Circular and equatorial: both the node and the argument of perigee are undefined; the true longitude (ClassicalElements::truelon) replaces them.

Trait Implementations

impl Clone for OrbitType

fn clone(&self) -> OrbitType

Returns a duplicate of the value.

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

Performs copy-assignment from source.

impl Copy for OrbitType

impl Debug for OrbitType

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

Formats the value using the given formatter.

impl Eq for OrbitType

impl PartialEq for OrbitType

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

Equality operator ==.

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

Inequality operator !=.

impl StructuralPartialEq for OrbitType