CubeSatDisturbanceAnalysis:

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
------------------------------------------------------------------------

Children:

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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