CubeSatGGStabilized:

Path: CubeSat/Simulation

% Demonstrate a CubeSat with gravity gradient stabilization.
  The gravity gradient boom is along the Z axis in the body frame, and
  produces restoring torques around X and Y. 
  ----------------------------------------------------------------------
  See also AnimQ, QForm, Plot2D, TimeLabl, RK4, Skew, Date2JD, 
  RHSCubeSat, BDipole
  ------------------------------------------------------------------------
%

Children:

AC: ACData/ACTConstants
AerospaceUtils: AtmosphericCalculations/AtmDens2
AerospaceUtils: AtmosphericCalculations/AtmJ70
AerospaceUtils: AtmosphericCalculations/BaromExp
AerospaceUtils: AtmosphericCalculations/DiffusionExp
AerospaceUtils: Coord/ECIToEF
AerospaceUtils: Coord/QIToBDot
AerospaceUtils: Coord/QLVLH
AerospaceUtils: Coord/R2LatLon
CubeSat: AttitudeControl/InertiaCubeSat
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
Orbit: OrbitCoord/ConvertNORAD
Orbit: OrbitCoord/SLR
Orbit: OrbitMechanics/NORAD
Orbit: OrbitMechanics/NORADToEl
Orbit: OrbitMechanics/PropagateTLE
Orbit: OrbitMechanics/RVOrbGen
Orbit: Visualization/OrbTrack
SC: Attitude/LibrationFrequency
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/OrbRate
SC: BasicOrbit/Period
SC: BasicOrbit/RV2El
SC: BasicOrbit/RVFromKepler
SC: BasicOrbit/VOrbit
SC: Disturbances/GravityGradientFromR
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/SwooshWatermark
Common: CommonData/xSplashSmall
Common: ComponentModels/Box
Common: Control/C2DZOH
Common: Database/Constant
Common: FileUtils/FindDirectory
Common: General/CellToMat
Common: General/DeBlankLT
Common: General/DeleteCell
Common: General/DispWithTitle
Common: General/MatToCell
Common: General/Watermark
Common: Graphics/AddFillToPlots
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/TimeLabl
Common: Graphics/TitleS
Common: Graphics/XLabelS
Common: Graphics/YLabelS
Common: Graphics/ZLabelS
Common: MassProperties/AddMass
Common: MassProperties/IC623X3
Common: MassProperties/Inertias
Common: MassProperties/MassStructure
Common: Quaternion/AnimQ
Common: Quaternion/Mat2Q
Common: Quaternion/Q2Mat
Common: Quaternion/QForm
Common: Quaternion/QMult
Common: Quaternion/QPose
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: Integration/RK4
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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