Commit ddcfffa1 authored by Bryan Cazabonne's avatar Bryan Cazabonne
Browse files

Updated documentation.

parent a5a18818
......@@ -126,7 +126,7 @@ want to use the estimated covariance and state vector of an orbit determination
the results of the daily orbit determination.
The two batch least squares estimator implementations in Orekit are compatible to work with a `NumericalPropagator`, a
`DSSTPropagator`, or a `TLEPropagator`.
`DSSTPropagator`, a `TLEPropagator`, an `EcksteinHechlerPropagator`, or a `BrouwerLyddanePropagator`.
### Kalman filter
......@@ -206,7 +206,7 @@
* measurements parameters estimation (biases, satellite clock offset, station clock offset,
station position, pole motion and rate, prime meridian correction and rate, total zenith
delay in tropospheric correction)
* can be used with numerical, DSST, or SDP4/SGP4 propagators
* can be used with numerical, DSST, SDP4/SGP4, Eckstein-Hechler, or Brouwer-Lyddane propagators
* multi-satellites orbit determination
* initial orbit determination methods (Gibbs, Gooding, Lambert and Laplace)
* ground stations displacements due to solid tides
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