Struct sbp::messages::observation::msg_ephemeris_gps_dep_f::MsgEphemerisGpsDepF

pub struct MsgEphemerisGpsDepF {

    pub sender_id: Option<u16>,
    pub common: EphemerisCommonContentDepB,
    pub tgd: f64,
    pub c_rs: f64,
    pub c_rc: f64,
    pub c_uc: f64,
    pub c_us: f64,
    pub c_ic: f64,
    pub c_is: f64,
    pub dn: f64,
    pub m0: f64,
    pub ecc: f64,
    pub sqrta: f64,
    pub omega0: f64,
    pub omegadot: f64,
    pub w: f64,
    pub inc: f64,
    pub inc_dot: f64,
    pub af0: f64,
    pub af1: f64,
    pub af2: f64,
    pub toc: GpsTimeSec,
    pub iode: u8,
    pub iodc: u16,
}

Deprecated

This observation message has been deprecated in favor of ephemeris message using floats for size reduction.

Fields

sender_id: Option<u16>

The message sender_id

common: EphemerisCommonContentDepB

Values common for all ephemeris types

tgd: f64

Group delay differential between L1 and L2

c_rs: f64

Amplitude of the sine harmonic correction term to the orbit radius

c_rc: f64

Amplitude of the cosine harmonic correction term to the orbit radius

c_uc: f64

Amplitude of the cosine harmonic correction term to the argument of latitude

c_us: f64

Amplitude of the sine harmonic correction term to the argument of latitude

c_ic: f64

Amplitude of the cosine harmonic correction term to the angle of inclination

c_is: f64

Amplitude of the sine harmonic correction term to the angle of inclination

dn: f64

Mean motion difference

m0: f64

Mean anomaly at reference time

ecc: f64

Eccentricity of satellite orbit

sqrta: f64

Square root of the semi-major axis of orbit

omega0: f64

Longitude of ascending node of orbit plane at weekly epoch

omegadot: f64

Rate of right ascension

w: f64

Argument of perigee

inc: f64

Inclination

inc_dot: f64

Inclination first derivative

af0: f64

Polynomial clock correction coefficient (clock bias)

af1: f64

Polynomial clock correction coefficient (clock drift)

af2: f64

Polynomial clock correction coefficient (rate of clock drift)

toc: GpsTimeSec

Clock reference

iode: u8

Issue of ephemeris data

iodc: u16

Issue of clock data

Trait Implementations

impl Clone for MsgEphemerisGpsDepF

fn clone(&self) -> MsgEphemerisGpsDepF

Returns a copy of the value.

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

Performs copy-assignment from source.

impl ConcreteMessage for MsgEphemerisGpsDepF

const MESSAGE_TYPE: u16 = 134u16

The message type.

const MESSAGE_NAME: &'static str = "MSG_EPHEMERIS_GPS_DEP_F"

The message name.

impl Debug for MsgEphemerisGpsDepF

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

Formats the value using the given formatter.

impl FriendlyName for MsgEphemerisGpsDepF

fn friendly_name() -> &'static str

impl From<MsgEphemerisGpsDepF> for Sbp

fn from(msg: MsgEphemerisGpsDepF) -> Self

Converts to this type from the input type.

impl PartialEq<MsgEphemerisGpsDepF> for MsgEphemerisGpsDepF

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

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

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.

impl SbpMessage for MsgEphemerisGpsDepF

fn message_name(&self) -> &'static str

Get the message name.

fn message_type(&self) -> u16

Get the message type.

fn sender_id(&self) -> Option<u16>

Get the sender_id if it is set.

fn set_sender_id(&mut self, new_id: u16)

Set the sender id.

fn encoded_len(&self) -> usize

Number of bytes this message will take on the wire.

fn friendly_name(&self) -> &'static str

Get friendly name associated with the message.

impl TryFrom<Sbp> for MsgEphemerisGpsDepF

type Error = TryFromSbpError

The type returned in the event of a conversion error.

fn try_from(msg: Sbp) -> Result<Self, Self::Error>

Performs the conversion.

impl StructuralPartialEq for MsgEphemerisGpsDepF