Function navtk::navutils::ecef_to_cen

• Defined in File navigation.hpp

Function Documentation

Matrix3 navtk::navutils::ecef_to_cen(const Vector3 &Pe)

Computes the DCM that rotates a vector from the NED frame to the ECEF frame ( \(\textbf{C}_\text{NED}^\text{ECEF}\)).

This DCM varies as a function of position, which in this function is provided as an ECEF position vector.

See also

Coordinate Frames for definitions of ECEF and NED frames.

See also

llh_to_cen()

Parameters

Pe – ECEF Position Vector at which \(\textbf{C}_\text{NED}^\text{ECEF}\) is desired: [x y z] (meters)

Returns

NED-to-ECEF DCM ( \(\textbf{C}_\text{NED}^\text{ECEF}\)).