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 earth 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, 2022 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 2023.1 Correct Julian date (spring equinox) -------------------------------------------------------------------------------
AerospaceUtils: Coord/QLVLH AerospaceUtils: Visualization/ShowCAD Orbit: OrbitMechanics/Period Orbit: OrbitSim/RVFromKepler SC: Disturbances/Disturbances SC: Environs/EarthEnvironment SC: Ephem/QSunPointing SC: Ephem/SunV1 SC: SCModels/TwoArraySC Common: GUIs/Figui Common: Time/FindSolsticeOrEquinox Common: Time/JD2Array
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