Struct sbp::messages::observation::MsgEphemerisGal [−][src]
pub struct MsgEphemerisGal {Show 26 fields
pub sender_id: Option<u16>,
pub common: EphemerisCommonContent,
pub bgd_e1e5a: f32,
pub bgd_e1e5b: 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: f64,
pub af1: f64,
pub af2: f32,
pub toc: GpsTimeSec,
pub iode: u16,
pub iodc: u16,
pub source: u8,
}
Expand description
Satellite broadcast ephemeris for Galileo
The ephemeris message returns a set of satellite orbit parameters that is used to calculate Galileo satellite position, velocity, and clock offset. Please see the Signal In Space ICD OS SIS ICD, Issue 1.3, December 2016 for more details.
Fields
sender_id: Option<u16>
The message sender_id
common: EphemerisCommonContent
Values common for all ephemeris types
bgd_e1e5a: f32
E1-E5a Broadcast Group Delay
bgd_e1e5b: f32
E1-E5b Broadcast Group Delay
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: f64
Polynomial clock correction coefficient (clock bias)
af1: f64
Polynomial clock correction coefficient (clock drift)
af2: f32
Polynomial clock correction coefficient (rate of clock drift)
toc: GpsTimeSec
Clock reference
iode: u16
Issue of data (IODnav)
iodc: u16
Issue of data (IODnav). Always equal to iode
source: u8
0=I/NAV, 1=F/NAV
Trait Implementations
The message type.
The message name.
Performs the conversion.
Get the message name.
Get the message type.
Set the sender id.
Number of bytes this message will take on the wire.
Auto Trait Implementations
impl RefUnwindSafe for MsgEphemerisGal
impl Send for MsgEphemerisGal
impl Sync for MsgEphemerisGal
impl Unpin for MsgEphemerisGal
impl UnwindSafe for MsgEphemerisGal
Blanket Implementations
Mutably borrows from an owned value. Read more