Path: CubeSat/Demos/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 %
Common: Graphics/Plot2D Common: Quaternion/Q2Eul Common: Time/Date2JD CubeSat: MissionPlanning/AttitudeProfile CubeSat: MissionPlanning/ObservationTimeWindows CubeSat: MissionPlanning/ObservationTimeWindowsPlot CubeSat: Visualization/PlotOrbit SC: BasicOrbit/Period SC: BasicOrbit/RVFromKepler
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