Hi dialists,
 
Maybe this is an off-topic, but I found it in some gnomonics books and I'd like to know more about it:
 
It is well known that due to Kepler's Second Law the Earth (and any satellite) does not follow a circular
uniform movement but an elliptical non-uniform one. So the longitude of the Earth across the ecliptic is
not exactly proportional to time: the difference (True Longitude minus Mean Longitude) is called equation
of center 'c' and can be derived either solving Kepler's equation ( M = E - e*sin(E) ) or using an approximate
formula, something like
    c = (2e- 1/4*e^3)*sin(M) + 5/4*sin(2*M) + 13/12*e^3*sin(3*M)+ ...
where M, the mean anomaly, is the fraction of area swept by the Earth and e is the eccentricity of the orbit
(Yes, it's pre-copernican, but it works!).
 
OK, but which is the general _expression_ of this formula (for the n-th term) and where does it come from? Is
it a Fourier series or a Taylor series?  I've tried both and wasn't able to reach to any result like this.
 
Could anyone point me at some website where this series is derived?
 
Anselmo Perez Serrada

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