Note: Matlab Code must be done for this question, Do not solve it without MATLAB DOOOO NOT PLease

MATLAB CODE WITH PLOTS AND SCREENSHOTS MUST BE POSTED IN THE SOLUTION PLEASE.

DO NOT COPY-PASTE OTHERS SOLUTIONS PLEASE.

THE SOLUTION MUST INCLUDE THE TABLE BELOW. FILL IT PLEASE AND EXPLAIN HOW YOU FILL IT WITH MATLAB SCREENSHOTS.

Please: Include your MATLAB code below so I can copy paste the code and tested on the MATLAB program to make sure your code working 100%.

Asstgnment 1. For this assignment you will develop a MATLAB program that Section 6.3 describes orbit maneuvering. calculates the v budget for a Hohmann transfer between two Use the circular approximation for circular orbits, including an inclination change. The inputs will vind given by vind=2vsin(2i). be the altitudes of both circular orbits and the initial and final inclination angles. The program should calculate the minimum total v as well as the v components for each segment of the maneuver. Consider only circular to circular inclination changes. Pmanemer. Altitudes are in km and velocities 2. This table contains data to test your program. Run your program are in km/s using these inputs and fill in the missing information. I will further test your code with an additional set of inputs. Please make sure your code works for de-orbiting. (Transfers from larger radius to smaller radius orbits)