Question: Write a Matlab function to compute the time elapsed (t) since periapsis crossing, given; The mean orbit rate (n), The eccentricity (e), and the true
Write a Matlab function to compute the time elapsed (t) since periapsis crossing, given; The mean orbit rate (n), The eccentricity (e), and the true anomaly (). Test your function with the following inputs:
(a) n = 0.001, e = 0.01, = /2 rad.
(b) n = 0.00001, e = 0.3, = rad.
also write a short script to run the above tests
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