SOLVE IN MATLAB AND STEP BY STEP USING THE VALUES PROVIDED. ENCOUNTERED SEVERAL ERRORS AND ALL THE ANSWERS I GET EITHER DO NOT WORK OR ARE INCOMPLETE PLEASE.

You have to deliver a SW that solves the Lambert's problem; your input will be two observations given in Azimuth, Elevation and Range and the time

between these two observations.

Upload your code, it will be much appreciated if you upload a single $.$m or $.$py file $($or if you prefer a lightscript from matlab or a jupyter notebook for

python$).$

The code shall:

Convert from the topocentric horizon coordinate system $($azimuth$,$ elevation, range$)$ to the geocentric equatorial coordinates

Solve Lambert's problem from the two position vector and the time between them

Present the orbital parameter of the orbit

It would be good that the SW:

Uses a GUI

Plots the outcome orbit

Solve Lambert's problem from two position vector and time $($selection of input type$)$

You can use Matlab or Python; the code is expected to run on instructor's machine, please provide the dependencies of the SW$.$ You can use the

following coordinates $($Greenwich$)$: X$=1344\mathrm{.}143$kmY$=6068\mathrm{.}601$kmZ$=1429\mathrm{.}311$km