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(Elliptical orbit) Write a matlab code for the equation. Implement a numerical method to solve the differential equations. Generate the first 5 seconds of simulation.
(Elliptical orbit) Write a matlab code for the equation. 
Details rr()2=r2GM2r+r=0 Implement a numerical method to solve the differential equations. Generate the first 5 seconds of simulation. Assume a constant velocity v at t=0
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C++ Database Development
Authors: Al Stevens
1st Edition
1558283579, 978-1558283572
