Path: Orbit/RHSOrbit
% Computes the right hand side for Earth gravity with J2.
Uses a local version of AGravityC that explicitly uses only the J2 term.
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Form:
d = RHSGeoJ2; % default data
xDot = RHSGeoJ2( x, t, d, aExt )
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Inputs
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x (6,1) Position vector [rECI (km); vECI (km)];
t (1,1) Time since start Julian Date (s)
d (.) Gravity model struct
.j2 (1,2) J2 term (unnormalized and positive)
.mu (1,1) Spherical gravitational potential
.a (1,1) Planet radius
.jD0 (1,1) Start Julian Date
aExt (3,1) External acceleration vector [x;y;z] ECI
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Outputs
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xDot (6,1) [rDot;vDot]
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See also: ECIToEF, RHSGeoHarm
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AerospaceUtils: Coord/ECIToEF Common: Time/JD2T
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