Enum nyx_space::dynamics::guidance::StateParameter

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pub enum StateParameter {
Show 50 variants AoL, AoP, Apoapsis, ApoapsisRadius, BdotR, BdotT, BLTOF, C3, Cd, Cr, Declination, DryMass, Epoch, EccentricAnomaly, Eccentricity, Energy, FlightPathAngle, FuelMass, GeodeticHeight, GeodeticLatitude, GeodeticLongitude, GuidanceMode, Hmag, HX, HY, HZ, HyperbolicAnomaly, Inclination, Isp, MeanAnomaly, Periapsis, PeriapsisRadius, Period, RightAscension, RAAN, Rmag, SemiParameter, SMA, SemiMinorAxis, Thrust, TrueAnomaly, TrueLongitude, VelocityDeclination, Vmag, X, Y, Z, VX, VY, VZ,
}
Expand description

Common state parameters

Variants§

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AoL

Argument of Latitude (deg)

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AoP

Argument of Periapse (deg)

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Apoapsis

Apoapsis, shortcut for TA == 180.0

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ApoapsisRadius

Radius of apoapsis (km)

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BdotR

B-Plane B⋅R

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BdotT

B-Plane B⋅T

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BLTOF

B-Plane LTOF

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C3

C_3 in (km/s)^2

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Cd

Coefficient of drag

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Cr

Coefficient of reflectivity

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Declination

Declination (deg) (also called elevation if in a body fixed frame)

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DryMass

Dry mass (kg)

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Epoch

The epoch of the state

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EccentricAnomaly

Eccentric anomaly (deg)

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Eccentricity

Eccentricity (no unit)

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Energy

Specific energy

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FlightPathAngle

Flight path angle (deg)

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FuelMass

fuel mass in kilograms

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GeodeticHeight

Geodetic height (km)

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GeodeticLatitude

Geodetic latitude (deg)

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GeodeticLongitude

Geodetic longitude (deg)

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GuidanceMode

Return the guidance mode of the spacecraft

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Hmag

Orbital momentum

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HX

X component of the orbital momentum vector

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HY

Y component of the orbital momentum vector

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HZ

Z component of the orbital momentum vector

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HyperbolicAnomaly

Hyperbolic anomaly (deg), only valid for hyperbolic orbits

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Inclination

Inclination (deg)

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Isp

Specific impulse (isp) in seconds

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MeanAnomaly

Mean anomaly (deg)

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Periapsis

Periapsis, shortcut for TA == 0.0

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PeriapsisRadius

Radius of periapse (km)

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Period

Orbital period (s)

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RightAscension

Right ascension (deg)

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RAAN

Right ascension of the ascending node (deg)

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Rmag

Norm of the radius vector

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SemiParameter

Semi parameter (km)

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SMA

Semi major axis (km)

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SemiMinorAxis

Semi minor axis (km)

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Thrust

Thrust (Newtons)

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TrueAnomaly

True anomaly

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TrueLongitude

True longitude

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VelocityDeclination

Velocity declination (deg)

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Vmag

Norm of the velocity vector (km/s)

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X

X component of the radius (km)

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Y

Y component of the radius (km)

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Z

Z component of the radius (km)

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VX

X component of the velocity (km/s)

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VY

Y component of the velocity (km/s)

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VZ

Z component of the velocity (km/s)

Implementations§

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impl StateParameter

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pub fn default_event_precision(&self) -> f64

Returns the default event finding precision in the unit of that parameter

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pub const fn is_b_plane(&self) -> bool

Returns whether this parameter is of the B-Plane kind

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pub const fn is_orbital(&self) -> bool

Returns whether this is an orbital parameter

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pub const fn is_for_spacecraft(&self) -> bool

Returns whether this parameter is only applicable to a spacecraft state

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pub const fn unit(&self) -> &'static str

Trait Implementations§

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impl Clone for StateParameter

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fn clone(&self) -> StateParameter

Returns a copy of the value. Read more
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fn clone_from(&mut self, source: &Self)

Performs copy-assignment from source. Read more
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impl Debug for StateParameter

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

Formats the value using the given formatter. Read more
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impl<'de> Deserialize<'de> for StateParameter

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

Deserialize this value from the given Serde deserializer. Read more
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impl Display for StateParameter

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

Formats the value using the given formatter. Read more
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impl FromStr for StateParameter

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type Err = NyxError

The associated error which can be returned from parsing.
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fn from_str(s: &str) -> Result<Self, Self::Err>

Parses a string s to return a value of this type. Read more
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impl PartialEq for StateParameter

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

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

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const CARDINALITY: usize = 50usize

Number of values of type Self. Read more
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fn next(&self) -> Option<Self>

Returns value following *self or None if this was the end. Read more
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fn previous(&self) -> Option<Self>

Returns value preceding *self or None if this was the beginning. Read more
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fn first() -> Option<Self>

Returns the first value of type Self. Read more
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fn last() -> Option<Self>

Returns the last value of type Self. Read more
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impl Serialize for StateParameter

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

Serialize this value into the given Serde serializer. Read more
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impl Copy for StateParameter

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impl StructuralPartialEq for StateParameter

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