Help with Matlab please!!
Write a Matlab program that converts from COEs (classical orbital elements) to position and velocity vectors. You need to handle special cases (i=0, e=0) through warning statements.
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Help with Matlab please!! Write a Matlab program that converts from.docx
1. Help with Matlab please!!
Write a Matlab program that converts from COEs (classical orbital elements) to position and velocity vectors. You
need to handle special cases (i=0, e=0) through warning statements.