Struct sbp::messages::observation::MsgEphemerisDepD [−][src]
pub struct MsgEphemerisDepD {Show 30 fields
pub sender_id: Option<u16>,
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 toe_tow: f64,
pub toe_wn: u16,
pub toc_tow: f64,
pub toc_wn: u16,
pub valid: u8,
pub healthy: u8,
pub sid: GnssSignalDep,
pub iode: u8,
pub iodc: u16,
pub reserved: u32,
}
Expand description
Satellite broadcast ephemeris
The ephemeris message returns a set of satellite orbit parameters that is used to calculate GPS satellite position, velocity, and clock offset. Please see the Navstar GPS Space Segment/Navigation user interfaces (ICD- GPS-200, Table 20-III) for more details.
Fields
sender_id: Option<u16>
The message sender_id
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)
toe_tow: f64
Time of week
toe_wn: u16
Week number
toc_tow: f64
Clock reference time of week
toc_wn: u16
Clock reference week number
valid: u8
Is valid?
healthy: u8
Satellite is healthy?
sid: GnssSignalDep
GNSS signal identifier
iode: u8
Issue of ephemeris data
iodc: u16
Issue of clock data
reserved: u32
Reserved field
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 MsgEphemerisDepD
impl Send for MsgEphemerisDepD
impl Sync for MsgEphemerisDepD
impl Unpin for MsgEphemerisDepD
impl UnwindSafe for MsgEphemerisDepD
Blanket Implementations
Mutably borrows from an owned value. Read more