I have converted the coordinates from ECEF to ECI. How to convert velocities also? Copy link Member ronisbrcommentedJul 19, 2018 Hi @Tarlan0001 , Currently, SatelliteToolbox.jl has functions to compute the rotation description (DCM or Quaternion) between the coordinate frames supported. Hence, ...
dcm=dcmeci2ecef(reduction,utc) calculates the position direction cosine matrix (ECI to ECEF) as a 3-by-3-by-M array. The calculation is based on the specified reduction method and Universal Coordinated Time (UTC). example dcm=dcmeci2ecef(reduction,utc,deltaAT) uses the difference between ...
[r_eci,v_eci,a_eci] = ecef2eci(___,Name,Value) calculates the position, velocity, and acceleration vectors at a higher precision using Earth orientation parameters. If Earth orientation parameters are not specified, the function sets them to 0. exampleExamples...
and the velocity of the body with respect to ECEF frame, expressed in body frame (‾‾Vb), angular rates of the body with respect to ECI frame, expressed in body frame (‾‾ωb). Earth rotation rate (‾‾ωe), and relative angular rates of the body with respect to north-...
dcm=dcmeci2ecef(reduction,utc)calculates the position direction cosine matrix (ECI to ECEF) as a 3-by-3-by-Marray. The calculation is based on the specified reduction method and Coordinated Universal Time (UTC). example dcm= dcmeci2ecef(reduction,utc,deltaAT)uses the difference between Inter...