Path: CubeSat/AttitudeControl
% CubeSat disturbance analysis with deployable solar panels Demonstrate how to use CubeSatDisturbanceAnalysis to calculate disturbances over an orbit. The spacecraft is nadir-pointing along a LEO orbit. This example uses a model with deployable solar panels. See also CubeSatModel, SolarCellPower, QLVLH, CubeSatDisturbanceAnalysis, RHSCubeSat, Period, RVFromKepler, Figui, Date2JD