Struct sbp::messages::observation::MsgEphemerisQzss[][src]

pub struct MsgEphemerisQzss {
Show 24 fields pub sender_id: Option<u16>, pub common: EphemerisCommonContent, pub tgd: f32, pub c_rs: f32, pub c_rc: f32, pub c_uc: f32, pub c_us: f32, pub c_ic: f32, pub c_is: f32, 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: f32, pub af1: f32, pub af2: f32, pub toc: GpsTimeSec, pub iode: u8, pub iodc: u16,
}
Expand description

Satellite broadcast ephemeris for QZSS

The ephemeris message returns a set of satellite orbit parameters that is used to calculate QZSS satellite position, velocity, and clock offset.

Fields

sender_id: Option<u16>

The message sender_id

common: EphemerisCommonContent

Values common for all ephemeris types

tgd: f32

Group delay differential between L1 and L2

c_rs: f32

Amplitude of the sine harmonic correction term to the orbit radius

c_rc: f32

Amplitude of the cosine harmonic correction term to the orbit radius

c_uc: f32

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

c_us: f32

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

c_ic: f32

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

c_is: f32

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: f32

Polynomial clock correction coefficient (clock bias)

af1: f32

Polynomial clock correction coefficient (clock drift)

af2: f32

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

Returns a copy of the value. Read more

Performs copy-assignment from source. Read more

The message type.

The message name.

Formats the value using the given formatter. Read more

Performs the conversion.

Get the message name.

Get the message type.

Get the sender_id if it is set.

Set the sender id.

Number of bytes this message will take on the wire.

The type returned in the event of a conversion error.

Performs the conversion.

Auto Trait Implementations

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Mutably borrows from an owned value. Read more

Performs the conversion.

Performs the conversion.

The resulting type after obtaining ownership.

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The type returned in the event of a conversion error.

Performs the conversion.

The type returned in the event of a conversion error.

Performs the conversion.