Question: Matlab Help - Fixed Point Recursion Kepler's equation in celestial mechanics is of the form: x = m + esina, where e, m are known

Matlab Help - Fixed Point Recursion

Matlab Help - Fixed Point Recursion Kepler's equation in celestial mechanics is

Kepler's equation in celestial mechanics is of the form: x = m + esina, where e, m are known parameters, and one would like to solve for the fixed point I, which physically represents "eccen- tric anomaly" -an angular variable that defines the position of a planet moving along an elliptic orbit. The known parameters satisfy 0

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