Path: SC/Disturbances
% Run the disturbance model for a spacecraft with two rotating arrays. Define the orbit a priori and call the disturbance model in batch. The sun vector is held constant. The spacecraft - body 1 - points at the sun while the arrays - bodies 2 and 3 - rotate to point at the sun. Before the disturbances are calculated, the orientation is visualized in a loop using DrawSCPlanPlugIn. ------------------------------------------------------------------------ See also Disturbances, BuildTwoArraySC, Q2Mat, QLVLH, Date2JD, Period, RVFromKepler, SunV1, EarthEnvironment ------------------------------------------------------------------------ % ------------------------------------------------------------------------------- Copyright (c) 1998-2003 Princeton Satellite Systems, Inc. All rights reserved. ------------------------------------------------------------------------------- Since version 5.5 (2003) 2016.1 Add visualization of Earth and Sun vectors with DrawSCPlanPlugIn to verify correct solar panel pointing 2022.1 Use EarthEnvironment which computes eclipses -------------------------------------------------------------------------------
AerospaceUtils: CAD/DrawSCPlanPlugIn AerospaceUtils: Coord/QLVLH SC: BasicOrbit/Period SC: BasicOrbit/RVFromKepler SC: Disturbances/Disturbances SC: Environs/EarthEnvironment SC: Ephem/SunV1 SC: SCModels/TwoArraySC Common: GUIs/Figui Common: Quaternion/Q2Mat Common: Time/Date2JD Common: Time/JD2Array
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