Path: CubeSat/AttitudeControl
% Example CubeSat disturbance analysis Demonstrate how to use CubeSatDisturbanceAnalysis to calculate disturbances over an orbit. The spacecraft is nadir-pointing along a LEO orbit. Some surfaces are given solar cell optical properties and some radiator properties. See also QLVLH, CubeSatDisturbanceAnalysis, RHSCubeSat, Period, RVFromKepler, OpticalSurfaceProperties, Figui, AU2Q, QMult, Date2JD