AttitudeProfileDemo:

Path: CubeSat/MissionPlanning

% Demonstrate the AttitudeProfile function.
 Plots the resulting quaternion and the separation angle from the
 secondary target.

  Mode 1:      Body y to Sun     (Body x to Nadir secondary)
  Mode 2:      Body x to Lat/Lon (Body y to Sun secondary)
  Mode 3:      Different Lat/Lon 

 See also AttitudeProfile, ObservationTimeWindows, PlotOrbit, Q2Eul, Plot2D,
 Date2JD, ObservationTimeWindowsPlot, Period, RVFromKepler
%