[][src]Struct mai400_api::rotating::KeplerElem

pub struct KeplerElem {
    pub semi_major_axis: f32,
    pub eccentricity: f32,
    pub inclination: f32,
    pub raan: f32,
    pub arg_parigee: f32,
    pub true_anomoly: f32,
}

Structure for keplarian elements returned in the standard telemetry message

Fields

Semi major axis (km)

Eccentricity

Inclination (deg)

Right ascension of ascending node (deg)

Argument of perigee (deg)

True anomaly (deg)

Trait Implementations

impl Default for KeplerElem
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impl PartialEq<KeplerElem> for KeplerElem
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impl Clone for KeplerElem
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Performs copy-assignment from source. Read more

impl Debug for KeplerElem
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Auto Trait Implementations

impl Send for KeplerElem

impl Sync for KeplerElem

Blanket Implementations

impl<T, U> Into for T where
    U: From<T>, 
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impl<T> ToOwned for T where
    T: Clone
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impl<T> From for T
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impl<T, U> TryFrom for T where
    T: From<U>, 
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🔬 This is a nightly-only experimental API. (try_from)

The type returned in the event of a conversion error.

impl<T> Borrow for T where
    T: ?Sized
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impl<T> Any for T where
    T: 'static + ?Sized
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impl<T, U> TryInto for T where
    U: TryFrom<T>, 
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🔬 This is a nightly-only experimental API. (try_from)

The type returned in the event of a conversion error.

impl<T> BorrowMut for T where
    T: ?Sized
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