Enum StateParameter

pub enum StateParameter {
    AoL,
    AoP,
    Apoapsis,
    ApoapsisRadius,
    BdotR,
    BdotT,
    BLTOF,
    C3,
    Cd,
    Cr,
    Declination,
    DryMass,
    Epoch,
    EccentricAnomaly,
    Eccentricity,
    Energy,
    FlightPathAngle,
    FuelMass,
    Height,
    Latitude,
    Longitude,
    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,
}

Common state parameters

Variants

AoL

Argument of Latitude (deg)

AoP

Argument of Periapse (deg)

Apoapsis

Apoapsis, shortcut for TA == 180.0

ApoapsisRadius

Radius of apoapsis (km)

BdotR

B-Plane B⋅R

BdotT

B-Plane B⋅T

BLTOF

B-Plane LTOF

C3

C_3 in (km/s)^2

Cd

Coefficient of drag

Cr

Coefficient of reflectivity

Declination

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

DryMass

Dry mass (kg)

Epoch

The epoch of the state

EccentricAnomaly

Eccentric anomaly (deg)

Eccentricity

Eccentricity (no unit)

Energy

Specific energy

FlightPathAngle

Flight path angle (deg)

FuelMass

fuel mass in kilograms

Height

Geodetic height (km)

Latitude

Geodetic latitude (deg)

Longitude

Geodetic longitude (deg)

GuidanceMode

Return the guidance mode of the spacecraft

Hmag

Orbital momentum

HX

X component of the orbital momentum vector

HY

Y component of the orbital momentum vector

HZ

Z component of the orbital momentum vector

HyperbolicAnomaly

Hyperbolic anomaly (deg), only valid for hyperbolic orbits

Inclination

Inclination (deg)

Isp

Specific impulse (isp) in seconds

MeanAnomaly

Mean anomaly (deg)

Periapsis

Periapsis, shortcut for TA == 0.0

PeriapsisRadius

Radius of periapse (km)

Period

Orbital period (s)

RightAscension

Right ascension (deg)

RAAN

Right ascension of the ascending node (deg)

Rmag

Norm of the radius vector

SemiParameter

Semi parameter (km)

SMA

Semi major axis (km)

SemiMinorAxis

Semi minor axis (km)

Thrust

Thrust (Newtons)

TrueAnomaly

True anomaly

TrueLongitude

True longitude

VelocityDeclination

Velocity declination (deg)

Vmag

Norm of the velocity vector (km/s)

X

X component of the radius (km)

Y

Y component of the radius (km)

Z

Z component of the radius (km)

VX

X component of the velocity (km/s)

VY

Y component of the velocity (km/s)

VZ

Z component of the velocity (km/s)

Implementations

impl StateParameter

pub fn default_event_precision(&self) -> f64

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

pub const fn is_b_plane(&self) -> bool

Returns whether this parameter is of the B-Plane kind

pub const fn is_orbital(&self) -> bool

Returns whether this is an orbital parameter

pub const fn is_for_spacecraft(&self) -> bool

Returns whether this parameter is only applicable to a spacecraft state

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

Trait Implementations

impl Clone for StateParameter

fn clone(&self) -> StateParameter

Returns a copy of the value.

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

Performs copy-assignment from source.

impl Debug for StateParameter

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

Formats the value using the given formatter.

impl<'de> Deserialize<'de> for StateParameter

fn deserialize<__D>(__deserializer: __D) -> Result<Self, __D::Error>

where __D: Deserializer<'de>,

Deserialize this value from the given Serde deserializer.

impl Display for StateParameter

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

Formats the value using the given formatter.

impl FromStr for StateParameter

type Err = NyxError

The associated error which can be returned from parsing.

fn from_str(s: &str) -> Result<Self, Self::Err>

Parses a string s to return a value of this type.

impl PartialEq for StateParameter

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

const CARDINALITY: usize = 50usize

Number of values of type Self.

fn next(&self) -> Option<Self>

Returns value following *self or None if this was the end.

fn previous(&self) -> Option<Self>

Returns value preceding *self or None if this was the beginning.

fn first() -> Option<Self>

Returns the first value of type Self.

fn last() -> Option<Self>

Returns the last value of type Self.

impl Serialize for StateParameter

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

where __S: Serializer,

Serialize this value into the given Serde serializer.

impl Copy for StateParameter

impl StructuralPartialEq for StateParameter