Path: Orbit/Interplanetary
% Calculate the heliocentric gravity for the position and date.
Julian date is only used if lunar gravitational harmonics are used.
If the field, sphHarmMoon, is not empty, it uses the moon harmonics.
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Form:
a = GravityHelio( r, jD, rP, mu, iD, d )
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Inputs
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r (3,1) Heliocentric position (km)
jD (1,1) Julian date (days)
rP (3,:) Heliocentric planet locations (km)
mu (1,:) Gravitational constants (km^3/s^2)
iD (1,:) JPL planet ids
d (.) Data structure
.muSun (1,1) Sun gravity constants
.sphHarmMoon (.) Data structure for the moon harmonics
.moonID (1,1) The index for the moon id in iD
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Outputs
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a (3,:) ECI force vector (N)
See also APlanet, AGravityC, MoonRot
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AC: ACData/ACTConstants Orbit: GravityModels/LoadGEM Orbit: GravityModels/NormalizationMatrix Orbit: OrbitMechanics/AGravityC Orbit: OrbitMechanics/APlanet SC: Ephem/MoonRot SC: SCData/sCTConstants SC: SCMat/GEMT1 Common: CommonData/Constants Common: CommonData/SwooshWatermark Common: CommonData/xSplashSmall Common: Database/Constant Common: General/CellToMat Common: General/DeBlankLT Common: General/DeleteCell Common: General/DispWithTitle Common: General/MatToCell Common: General/Watermark Common: Graphics/Mesh2 Common: Graphics/NewFig Common: Graphics/Plot2D Common: Graphics/PltStyle Common: Graphics/XLabelS Common: Graphics/YLabelS Common: Graphics/ZLabelS Math: Linear/DupVect Math: Linear/Factorl Math: Linear/Mag
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