please i want to know where is the mistake in the this code

[R,tof] = Q1_STNO(v,theta);
G=9.81;
R=Q1_0123456(v,theta);
R=(v^2)*sin(2*theta)/g;

tof=Q1_0123456(v,theta);
tof=2*v*sin(theta)/g;

disp([‘Answer = ‘ num2str(R)’]);
disp([‘Answer = ‘ num2str(theta)’]);

Answer 1

[Image Analyst]

Your quotes are messed up in the disp statement. Try it like this instead:

fprintf('R Answer = %f\n', R);
fprintf('theta Answer = %f\n', theta);

Answer 2

[Roger Stafford]

In the first line you compute R and tof. In the third and fourth lines you overwrite R. In the fifth and sixth lines you overwrite tof. This means that the first, the third, and the fifth lines of code are entirely ignored and accomplish nothing. What is it you actually wish to calculate?

Answer 3

[mohammad Mohsen]

thanks alot guys that you answer me

what iam looking for where is the launch angle and is the acceleration due to gravity? but still give me error in line 1

Undefined function or variable 'v'.

Error in part1 (line 1) [R,tof] = Q1_STNO(v,theta);

[Image Analyst]

So give a value to v before you call that function. How is it supposed to know what v is unless you tell it?

Answer 4

[mohammad Mohsen]

function f = Q1_0123456(v,theta)

[R,ToF] = Q1_STNO(v,theta);

g=9.81;

R=Q1_0123456(v,theta);

R=(v^2)*sin(2*theta)/g;

tof=Q1_0123456(100,30);

tof=2*v*sin(theta)/g;

fprintf('R Answer = %f\n', R);

fprintf('theta Answer = %f\n', theta);

this is how i wrote it and still have wrong run please help

[Image Analyst]

Is it your intent to call this recursively? Because Q1_0123456() calls itself from inside itself.

Answer 5

[mohammad Mohsen]

 [hMaxAir,hMaxVac] = Q2_STNO(v,theta);

 [x,y,range] = trajectoryInAir(v,theta);

 [x,y,range] = trajectoryInAir(100,40); 

 plot(x,y); 

 axis equal;

and this is second Question please check for me

calculate the maximum height reached by a cannonball both with and without drag due to air resistance

Answer 6

[mohammad Mohsen]

[vmin,vmax] = Q3_STNO(X,W);

vmin=Q3_0123456(X,W);

vmin=[x,y,range] = trajectoryInAir(0.1,0.5);

vmax=[x,y,range] = trajectoryInAir(0.5,1);

plot(x,y);

axis equal;

 and this is the third :)