please,

Below are the equations of State trajectories a1 and a2 obtained from the solution of a system's differential equation. a -) write a program that calculates the system's state trajectories (a1 and a2) in the range of T=1-5 seconds using for-end or while-end loops (the Workspace image is given below). (10p). b -) in the developed program, draw a1 and a2 state orbits in the range of T=1-5 seconds so that the horizontal axes(s) are a1 and a2, respectively, the vertical axes, as shown below (15 p).

a(t) A(t)= 1-2-2-' 2-e+e' Workspace Name Ja 1 Value a2 [-1.8536 -6.4074 - 19.0880-53.5985 - 147.4132] [4.7179 9.3891 22.0855 56.5982 150.4132] [1 2 3 4 5] 0 -50 (1) e -100 -150 1 1.5 N 2.5 3.5 4 4.5 5 3 zaman (s) 200 150 a(t) 100 50 0 1.5 N 2.5 3.5 4 4.5 5 zaman (s)