Struct JupiterSystemIII 

pub struct JupiterSystemIII;

Jupiter System III body-fixed frame.

Defined by Jupiter’s magnetic field rotation period (9h 55m 29.711s). Uses latitude/longitude/radius spherical naming.

Trait Implementations

impl Clone for JupiterSystemIII

fn clone(&self) -> JupiterSystemIII

Returns a duplicate of the value.

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

Performs copy-assignment from source.

impl Copy for JupiterSystemIII

impl Debug for JupiterSystemIII

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

Formats the value using the given formatter.

impl Default for JupiterSystemIII

fn default() -> JupiterSystemIII

Returns the “default value” for a type.

impl<'de> Deserialize<'de> for JupiterSystemIII

fn deserialize<__D>( __deserializer: __D, ) -> Result<JupiterSystemIII, <__D as Deserializer<'de>>::Error>

where __D: Deserializer<'de>,

Deserialize this value from the given Serde deserializer.

impl Eq for JupiterSystemIII

impl FrameRotationProvider<EME2000, JupiterSystemIII> for ()

fn rotation<Eph, Eop: EopProvider, Nut: NutationModel>( jd: JulianDate, ctx: &AstroContext<Eph, Eop>, ) -> Rotation3

Computes the rotation matrix from frame F1 to frame F2.

impl FrameRotationProvider<EclipticMeanJ2000, JupiterSystemIII> for ()

fn rotation<Eph, Eop: EopProvider, Nut: NutationModel>( jd: JulianDate, ctx: &AstroContext<Eph, Eop>, ) -> Rotation3

Computes the rotation matrix from frame F1 to frame F2.

impl FrameRotationProvider<ICRS, JupiterSystemIII> for ()

fn rotation<Eph, Eop: EopProvider, Nut: NutationModel>( jd: JulianDate, ctx: &AstroContext<Eph, Eop>, ) -> Rotation3

Computes the rotation matrix from frame F1 to frame F2.

impl FrameRotationProvider<JupiterSystemIII, EME2000> for ()

fn rotation<Eph, Eop: EopProvider, Nut: NutationModel>( jd: JulianDate, ctx: &AstroContext<Eph, Eop>, ) -> Rotation3

Computes the rotation matrix from frame F1 to frame F2.

impl FrameRotationProvider<JupiterSystemIII, EclipticMeanJ2000> for ()

fn rotation<Eph, Eop: EopProvider, Nut: NutationModel>( jd: JulianDate, ctx: &AstroContext<Eph, Eop>, ) -> Rotation3

Computes the rotation matrix from frame F1 to frame F2.

impl FrameRotationProvider<JupiterSystemIII, ICRS> for ()

fn rotation<Eph, Eop: EopProvider, Nut: NutationModel>( jd: JulianDate, _ctx: &AstroContext<Eph, Eop>, ) -> Rotation3

Computes the rotation matrix from frame F1 to frame F2.

impl PartialEq for JupiterSystemIII

fn eq(&self, other: &JupiterSystemIII) -> 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 ReferenceFrame for JupiterSystemIII

fn frame_name() -> &'static str

Returns the canonical name of this reference frame.

fn spherical_names() -> Option<(&'static str, &'static str, &'static str)>

Returns frame-specific names for spherical coordinate components.

impl Serialize for JupiterSystemIII

fn serialize<__S>( &self, __serializer: __S, ) -> Result<<__S as Serializer>::Ok, <__S as Serializer>::Error>

where __S: Serializer,

Serialize this value into the given Serde serializer.

impl SphericalNaming for JupiterSystemIII

fn polar_name() -> &'static str

Returns the name for the polar/elevation angle (e.g., “dec”, “lat”, “alt”, “b”).

fn azimuth_name() -> &'static str

Returns the name for the azimuthal angle (e.g., “ra”, “lon”, “az”, “l”).

fn distance_name() -> &'static str

Returns the name for the radial distance (e.g., “distance”, “altitude”, “radius”).

impl StructuralPartialEq for JupiterSystemIII