Path: Orbit/RHSOrbit
% Right-hand-side for equinoctial elements.
--------------------------------------------------------------------------
Form:
d = RHSEquinoctial
xDot = RHSEquinoctial( t, x, d )
--------------------------------------------------------------------------
------
Inputs
------
t (1,1) Time
x (6,1) States [p;f;g;h;k;L]
d (.) Structure to pass to the integration RHS
.mu (1,1)
.f (3,1) Acceleration vector
-------
Outputs
-------
xDot (6,1) State derivatives d[p;f;g;h;k;L]/dt
a (6,6) a matrix
--------------------------------------------------------------------------
Common: Database/Constant
Back to the Orbit Module page