In Matlab, add J2 perturbations to your two body propagation. Comment on your findings. Also, how would you change your code if you had other things affecting the orbit. For example, solar radiation pressure, third body perturbations, or drag. Do you just add the accelerations together in the function?

In Matlab, add J2 perturbations to your two body propagation. Comment on your findings. Also, how would you change your code if you had other things affecting the orbit. For example, solar radiation pressure, third body perturbations, or drag. Do you just add the accelerations together in the function?

Elements Of Electromagnetics

7th Edition

ISBN:9780190698614

Author:Sadiku, Matthew N. O.

Publisher:Sadiku, Matthew N. O.

ChapterMA: Math Assessment

Section: Chapter Questions

Problem 1.1MA

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