Path: Orbit/RHSOrbit
% Computes the right hand side of the variational equations.
Since version 1.
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Form:
xDot = FVarEq( x, t, eType, aD, tol, mu )
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Inputs
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x Elements vector [a;i;W;w;e;M] or [a;P1;P2;Q1;Q2;l]
t Current time (for use with RK4)
eType 'eqt','eqp','elt','elp' where
'eq' --> equinoctial
'el' --> elements (Gauss formulation)
't' --> tangential
'p' --> polar
aD Disturbance vector [tangent;normal;z]
tol Tolerance for Kepler's equation solver
mu Gravitational parameter
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Outputs
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xDot Derivative of the elements
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Orbit: OrbitCoord/CT2REq Orbit: OrbitCoord/K2L Orbit: OrbitCoord/ML2K Orbit: OrbitCoord/ML2KApp Orbit: OrbitMechanics/VarEqP Orbit: OrbitMechanics/VarEqT Orbit: OrbitMechanics/VarGausP Orbit: OrbitMechanics/VarGausT SC: BasicOrbit/E2Nu SC: BasicOrbit/M2EApp SC: BasicOrbit/M2EEl Common: CommonData/SwooshWatermark Common: General/CellToMat Common: General/MatToCell Common: General/Watermark Common: Graphics/NewFig Common: Graphics/Plot2D Common: Graphics/PltStyle Math: Linear/DupVect
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