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solving Kepler's equation using Danby's method
11-03-2016, 05:30 PM
Post: #1
solving Kepler's equation using Danby's method
This HP Prime program demonstrates how to solve Kepler's equation for elliptical and hyperbolic orbits using Professor Danby's numerical method.

Here is the output from this program.

demo_kepler1

mean anomaly = 79.4849999996 degrees

eccentricity = 1.735

true anomaly = 91.4538050798 degrees

The attached zip file also includes a PDF document which provides additional information about the implementation.


Attached File(s)
.zip  demo_kepler1.zip (Size: 287.71 KB / Downloads: 5)
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