CubeSatLunarEnvironment:
% Lunar environment calculations for the CubeSat dynamical model.
Computes sun location with SunV1 and accounts for eclipses from the Earth and
the Moon via Eclipse. All environment constants including gravity are defined
here.
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Form:
d
e = CubeSatLunarEnvironment( x, t, d )
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Inputs
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x (14,1) [r;v;q;w;b]
t (1,1) Time, sec
d (.) Data structure
.jD0 Julian date of epoch
.surfData (.) optional; empty to skip optical calcs
.gravity (.)
.center Index of gravity center
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Outputs
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env (.) Environmental data
.r ECI position (km)
.v ECI velocity (km/s)
.q ECI to body quaternion
.mu Gravitational constant (km3/s2)
.radiusPlanet Radius of the center planet (km)
.rho Distance from the Moon (km)
.radiation Planetary radiation W/m2
.albedo Planet bond albedo fraction
.uSun Sun unit vector (ECI)
.rSun Sun distance (km)
.solarFlux Solar flux at position (W/m2)
.nEcl Eclipse fraction (source intensity, 0-1)
.accelGrav Acceleration due to gravity
.rMoon Moon position
.vMoon Moon velocity
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See also SunV1, Eclipse, AtmDens2, AtmJ70, BDipole
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Children:
AeroUtils: Coord/QLVLH
Common: General/CellToMat
Common: General/DeBlankLT
Common: General/MatToCell
Common: General/Watermark
Common: Graphics/NPlot
Common: Graphics/NewFig
Common: Graphics/Plot2D
Common: Graphics/PltStyle
Common: Graphics/XLabelS
Common: Graphics/YLabelS
Common: Quaternion/Mat2Q
Common: Quaternion/QMult
Common: Time/DTSToDTA
Common: Time/Date2JD
Common: Time/JD2000
CubeSat: Utilities/CubeSatAttitude
Math: Linear/Cross
Math: Linear/Dot
Math: Linear/DupVect
Math: Linear/Mag
Math: Linear/Unit
Orbit: GravityModels/GravityNormalized
Orbit: GravityModels/NormalizationMatrix
Orbit: GravityModels/UnnormalizeGravity
Orbit: OrbitMechanics/AGravityC
Orbit: OrbitMechanics/APlanet
SC: Ephem/CEcl2Eq
SC: Ephem/Eclipse
SC: Ephem/InterpolateState
SC: Ephem/MoonRot
SC: Ephem/PlanetPosJPL
