Struct Epoch 

pub struct Epoch {
    pub references: Vec<SatMeas>,
    pub nonref: Vec<SatMeas>,
    pub velocity_mps: Option<[f64; 3]>,
    pub dt_s: f64,
}

One RTK epoch: the per-system double-difference reference satellites present this epoch plus the non-reference satellites observed at both receivers. Each non-reference satellite differences against the reference of its own system (the first byte of the satellite id); a one-element references is the historical single-system epoch.

Fields

references: Vec<SatMeas>

nonref: Vec<SatMeas>

velocity_mps: Option<[f64; 3]>

Optional rover ECEF velocity in metres/second for the velocity-propagated predict branch. The value is an epoch input, not carried filter state.

dt_s: f64

Elapsed seconds since the previous filter epoch, used only when crate::rtk_filter::UpdateOpts::dynamics_model is crate::rtk_filter::DynamicsModel::VelocityPropagated.

Trait Implementations

impl Clone for Epoch

fn clone(&self) -> Epoch

Returns a duplicate of the value.

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

Performs copy-assignment from source.

impl Debug for Epoch

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

Formats the value using the given formatter.

impl PartialEq for Epoch

fn eq(&self, other: &Epoch) -> bool

Equality operator ==.

fn ne(&self, other: &Rhs) -> bool

Inequality operator !=.

impl StructuralPartialEq for Epoch