function [] = model_rocket_townsenm(v_rocket, theta)
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%
%  Programmer(s) and Purdue Email Address(es):Matthew Townsend
%  1. townsenm@purdue.edu
%
%  Section #:017
%
%  Assignment #:5
%
%  Academic Integrity Statement:
%
%       I/We have not used source code obtained from
%       any other unauthorized source, either modified
%       or unmodified.  Neither have I/we provided access
%       to my/our code to another. The project I/we am/are
%       submitting is my/our own original work.
%
% FUNCTION NAME: model_rocket_townsenm
% INPUTS: List them below one line per input argument
%  v_rocket, the intial velocity of the rocket.
%  theta, the angle of elevation that the rocket will be propelled.
% OUTPUTS: List them below line per output argument
% the ouputs are the different heigths at each sencond
%
% The purpose of this function is to map the heigth of a rocket given theta
% and velocity of the rocket at each second.
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t=0; %this is the starting time for t
y=0; %this is the intial height where heigth will begin at 0.
fprintf('For an intial velocity (m/s) of %6.2f and angle of %6.2f degrees \n',v_rocket,theta)
while y >= 0  %heigth must be above 0 in order for the
    dist = (v_rocket*cos(theta))*t; %this is the calculations for distance in meters
    y = (v_rocket*sin(theta))*t-((1/2)*(9.81)*(t^2)); %this is the calculations for height in meters
    fprintf('AT %6.2f seconds, the heigth is %6.2f m and distance is %6.2f m \n',t,y,dist)
    t = t + 1; %this increases time by one second for each loop.
end