Struct sbp::messages::observation::MsgEphemerisBds

pub struct MsgEphemerisBds {

    pub sender_id: Option<u16>,
    pub common: EphemerisCommonContent,
    pub tgd1: f32,
    pub tgd2: 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: f32,
    pub af2: f32,
    pub toc: GpsTimeSec,
    pub iode: u8,
    pub iodc: u16,
}

Satellite broadcast ephemeris for BDS

The ephemeris message returns a set of satellite orbit parameters that is used to calculate BDS satellite position, velocity, and clock offset. Please see the BeiDou Navigation Satellite System SIS-ICD Version 2.1, Table 5-9 for more details.

Fields

sender_id: Option<u16>

The message sender_id

common: EphemerisCommonContent

Values common for all ephemeris types

tgd1: f32

Group delay differential for B1

tgd2: f32

Group delay differential for B2

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: 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 Calculated from the navigation data parameter t_oe per RTCM/CSNO recommendation: IODE = mod (t_oe / 720, 240)

iodc: u16

Issue of clock data Calculated from the navigation data parameter t_oe per RTCM/CSNO recommendation: IODE = mod (t_oc / 720, 240)

Trait Implementations

impl Clone for MsgEphemerisBds

fn clone(&self) -> MsgEphemerisBds

Returns a copy of the value.

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

Performs copy-assignment from source.

impl ConcreteMessage for MsgEphemerisBds

const MESSAGE_TYPE: u16

The message type.

const MESSAGE_NAME: &'static str

The message name.

impl Debug for MsgEphemerisBds

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

Formats the value using the given formatter.

impl From<MsgEphemerisBds> for Sbp

fn from(msg: MsgEphemerisBds) -> Self

Performs the conversion.

impl SbpMessage for MsgEphemerisBds

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.

impl TryFrom<Sbp> for MsgEphemerisBds

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.