Path: CubeSat/Visualization
% Plot the state in 3D with an Earth map.
Note that the location relative to the map is only accurate for
Earth-fixed frame input. Enter time and Julian date to compute the
Earth-fixed positions from ECI data automatically.
--------------------------------------------------------------------------
Form:
[h, l] = PlotOrbit( rEF )
[h, l] = PlotOrbit( rECI, t, jD0 )
--------------------------------------------------------------------------
------
Inputs
------
r (3,m) Position vectors (km)
or
{n} Cell array of position matrices for multiple satellites
t (1,:) Time array (sec)
jD0 (1,1) Epoch Julian date
------
Output
------
h (1,1) Figure handle
l (1,n) Handle to orbit lines
--------------------------------------------------------------------------
See also: LoadEarthMap
--------------------------------------------------------------------------
AerospaceUtils: Coord/ECIToEF SC: Visualization/LoadEarthMap Common: Time/JD2T
Back to the CubeSat Module page