public static class OrbitModel.Quadrature extends Object
dv/dt=-Ksin(ω+ν)*dν/dt=0to
ω+ν=0. (dν/dt &neq; 0)From
M=E-e·sin(E) and
tan(ν/2)=±1 = sqrt((1+e)/(1-e))·tan(E/2) it follows
Φ=(t-t_0)/P=(E-e·sin(E))/2π
| Constructor and Description |
|---|
Quadrature() |
| Modifier and Type | Method and Description |
|---|---|
static void |
main(String[] arg)
First argument is the time of perihelion passage, t_0, second is
eccentricity.
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public static void main(String[] arg)