Sgp4PropagatorEstimateElements Method |
Overload List| Name | Description | |
|---|---|---|
  | EstimateElements(DateMotionCollectionCartesian, Sgp4PropagatorSgp4EstimationInput) |
Produces a batch least squares fit for a given set of trajectory observations (states).
This overload will take the first position and velocity after the RequestedEstimationEpoch
in the ephemerisInTEME and use the MeanElementsAtEpoch(JulianDate, Cartesian, Cartesian) to
produce an initial guess.
|
| EstimateElements(DateMotionCollectionCartesian, Cartesian, Cartesian, Sgp4PropagatorSgp4EstimationInput) |
Produces a batch least squares fit for a given set of trajectory observations (states). The specified position and velocity
provide the values to use as the state expected at the RequestedEstimationEpoch in the configuration.
The estimation takes this state and uses MeanElementsAtEpoch(JulianDate, Cartesian, Cartesian) to
produce an initial guess for the least squares.
|
See Also