Path: Orbit/GravityModels
% Computes the acceleration due to the Sun and the Earth/Moon. The position is in the Sun-Earth/Moon frame. Type SEMGravAcc for a built-in demo creating gravity contour plots. Since version 10. -------------------------------------------------------------------------- Form: [gSun,gEM,gCompare] = SEMGravAcc( rSEM ) -------------------------------------------------------------------------- ------ Inputs ------ rSEM (2,:) Position vector in SEM frame ------- Outputs ------- gSun (:,:) Gravitational acceleration due to the Sun gEM (:,:) Gravitational acceleration due to the Earth/Moon gCompare (:,:) gEM/gSun --------------------------------------------------------------------------
AC: ACData/ACTConstants SC: SCData/sCTConstants Common: CommonData/Constants Common: CommonData/xSplashSmall Common: Database/Constant Common: General/DeleteCell Common: Graphics/NewFig
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