Struct sbp::messages::observation::msg_ephemeris_gps::MsgEphemerisGps
source · pub struct MsgEphemerisGps {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 GPS
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
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§
source§impl Clone for MsgEphemerisGps
impl Clone for MsgEphemerisGps
source§fn clone(&self) -> MsgEphemerisGps
fn clone(&self) -> MsgEphemerisGps
1.0.0 · source§fn clone_from(&mut self, source: &Self)
fn clone_from(&mut self, source: &Self)
source
. Read moresource§impl ConcreteMessage for MsgEphemerisGps
impl ConcreteMessage for MsgEphemerisGps
source§const MESSAGE_TYPE: u16 = 138u16
const MESSAGE_TYPE: u16 = 138u16
source§const MESSAGE_NAME: &'static str = "MSG_EPHEMERIS_GPS"
const MESSAGE_NAME: &'static str = "MSG_EPHEMERIS_GPS"
source§impl Debug for MsgEphemerisGps
impl Debug for MsgEphemerisGps
source§impl<'de> Deserialize<'de> for MsgEphemerisGps
impl<'de> Deserialize<'de> for MsgEphemerisGps
source§fn deserialize<__D>(__deserializer: __D) -> Result<Self, __D::Error>where
__D: Deserializer<'de>,
fn deserialize<__D>(__deserializer: __D) -> Result<Self, __D::Error>where
__D: Deserializer<'de>,
source§impl FriendlyName for MsgEphemerisGps
impl FriendlyName for MsgEphemerisGps
fn friendly_name() -> &'static str
source§impl From<MsgEphemerisGps> for Sbp
impl From<MsgEphemerisGps> for Sbp
source§fn from(msg: MsgEphemerisGps) -> Self
fn from(msg: MsgEphemerisGps) -> Self
source§impl PartialEq for MsgEphemerisGps
impl PartialEq for MsgEphemerisGps
source§fn eq(&self, other: &MsgEphemerisGps) -> bool
fn eq(&self, other: &MsgEphemerisGps) -> bool
self
and other
values to be equal, and is used
by ==
.