Path: CubeSat/AttitudeControl
% CubeSat disturbance analysis from batch data using RHSCubeSat. Compute the drag, magnetic, gravity gradient, and optical disturbances. The environment is computed using AtmJ70, BDipole, and SunV1. AtmDens2 can be used instead by supplying an empty matrix for d.atm. The built-in demo computes the disturbances on a 3U satellite for one day. The center of mass is assumed to be offset from the geometric center of the spacecraft by a few cm. Note the growth in momentum. the gravity gradient torque is zero in the demo because the attitude entered is perfect LVLH and the inertia is symmetric. ------------------------------------------------------------------------ Form: [tT, fECI, h, hECI, f, t, power] = CubeSatDisturbanceAnalysis( d, q, r, v, jD ) CubeSatDisturbanceAnalysis % demo ------------------------------------------------------------------------ ------ Inputs ------ d (.) Data structure from RHSCubeSat q (4,:) Quaternion, ECI to body r (3,:) Position vector v (3,:) Velocity vector jD (1,:) Julian dates ------- Outputs ------- tT (3,:) Torque in body (Nms) fECI (3,:) Force in ECI (N) h (3,:) Body momentum (Nms) hECI (3,:) ECI momentum (Nms) torque (.) Torque structure .total (3,:) Torque in body frame .aero (3,:) Aerodynamic torque .mag (3,:) Magnetic torque .optical (3,:) Optical torque .gg (3,:) Gravity gradient torque force (.) Force structure .total (3,:) Force in ECI frame .aero (3,:) Aerodynamic force .optical (3,:) Optical force ------------------------------------------------------------------------ See also CubeSatAero, CubeSatRadiationPressure, GravityGradientFromR, RHSCubeSat ------------------------------------------------------------------------
AC: ACData/ACTConstants AerospaceUtils: AtmosphericCalculations/AtmDens2 AerospaceUtils: AtmosphericCalculations/AtmJ70 AerospaceUtils: AtmosphericCalculations/BaromExp AerospaceUtils: AtmosphericCalculations/DiffusionExp AerospaceUtils: CAD/GenericProperties AerospaceUtils: Coord/ECIToEF AerospaceUtils: Coord/QIToBDot AerospaceUtils: Coord/QLVLH AerospaceUtils: Coord/R2LatLon CubeSat: Power/SolarCellPower CubeSat: Simulation/CubeSatAero CubeSat: Simulation/CubeSatEnvironment CubeSat: Simulation/CubeSatRadiationPressure CubeSat: Simulation/RHSCubeSat CubeSat: Utilities/CubeSatAttitude CubeSat: Utilities/CubeSatFaces CubeSat: Utilities/CubeSatModel CubeSat: Visualization/DrawCubeSat CubeSat: Visualization/GroundTrack FormationFlying: Help/HelpSystem Orbit: OrbitCoord/ConvertNORAD Orbit: OrbitCoord/SLR Orbit: OrbitMechanics/NORAD Orbit: OrbitMechanics/NORADToEl Orbit: OrbitMechanics/PropagateTLE Orbit: OrbitMechanics/RVOrbGen Orbit: Visualization/OrbTrack SC: BasicOrbit/CP2I SC: BasicOrbit/E2M SC: BasicOrbit/E2Nu SC: BasicOrbit/El2RV SC: BasicOrbit/M2E SC: BasicOrbit/M2EApp SC: BasicOrbit/M2EEl SC: BasicOrbit/M2EHy SC: BasicOrbit/M2Nu SC: BasicOrbit/M2NuPb SC: BasicOrbit/Nu2E SC: BasicOrbit/Nu2M SC: BasicOrbit/Period SC: BasicOrbit/RV2El SC: BasicOrbit/RVFromKepler SC: Disturbances/GravityGradientFromR SC: Disturbances/OpticalSurfaceProperties SC: Disturbances/SolarF SC: Environs/BDipole SC: Environs/SolarFluxPrediction SC: Ephem/ECIToPlanet SC: Ephem/EOfE SC: Ephem/EarthNut SC: Ephem/EarthPre SC: Ephem/EarthRot SC: Ephem/EarthRte SC: Ephem/Eclipse SC: Ephem/GMSTime SC: Ephem/MSidDay SC: Ephem/MoonRot SC: Ephem/Moons SC: Ephem/NutDelta SC: Ephem/ObOfE SC: Ephem/SunV1 SC: Ephem/TruEarth SC: SCData/sCTConstants SC: SCMat/EarthMR SC: SCMat/SolarFluxPredictions SC: Visualization/PlotPlanet SCPro: MannedVehicle/ISSOrbit Common: CommonData/Constants Common: CommonData/Sosumi Common: CommonData/SwooshWatermark Common: CommonData/xSplashSmall Common: ComponentModels/Box Common: Control/C2DZOH Common: Database/Constant Common: FileUtils/FindDirectory Common: GUIs/Figui Common: GUIs/MessageQueue Common: General/CellToMat Common: General/CloseFigure Common: General/DeBlankLT Common: General/DeleteCell Common: General/DispWithTitle Common: General/FSWClock Common: General/ListCases Common: General/MatToCell Common: General/Watermark Common: Graphics/AddFillToPlots Common: Graphics/AxesCart Common: Graphics/Axis3D Common: Graphics/DrawVertices Common: Graphics/Ellipsd Common: Graphics/Map Common: Graphics/Mesh2 Common: Graphics/NPlot Common: Graphics/NewFig Common: Graphics/Plot2D Common: Graphics/Plot3D Common: Graphics/PltStyle Common: Graphics/SortFigs Common: Graphics/TimeLabl Common: Graphics/TitleS Common: Graphics/XLabelS Common: Graphics/YLabelS Common: Graphics/ZLabelS Common: MassProperties/AddMass Common: MassProperties/IC623X3 Common: MassProperties/Inertias Common: Quaternion/AU2Q Common: Quaternion/Mat2Q Common: Quaternion/QForm Common: Quaternion/QMult Common: Quaternion/QTForm Common: Time/DTAToDTS Common: Time/DTSToDTA Common: Time/Date2DN Common: Time/Date2JD Common: Time/JD2000 Common: Time/JD2Array Common: Time/JD2DN Common: Time/JD2Date Common: Time/JD2T Common: Time/JDToMidnight Common: Time/T2JD Math: Linear/Cross Math: Linear/Dot Math: Linear/DupVect Math: Linear/Mag Math: Linear/Skew Math: Linear/SkewSq Math: Linear/SkewSymm Math: Linear/Unit Math: MathUtils/R2P5 Math: Trigonometry/ACosD Math: Trigonometry/CosD Math: Trigonometry/SinD
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