Using finite differences to find the displacement (x,y) of a projectile including the effect of drag

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When i enter the code below I get the following error:
Index exceeds the number of array elements (2).
Error in EGB211_CLA (line 37)
XxNow = XxN(i-1) ;
Would anyone know how to fix this issue? My code is below as well
close all
clc
%% Problem Parameters
m = 0.05 ; % mass (kg) = 50x10^-3
angle = 25 ; % initial angle (degrees)
th0 = angle*(pi/180) ; % initial angle (radians)
Xx0 = 0 ; % initial horizontal displacement (m)
Xy0 = 50 ; % initial vertical displacement (m)
V0 = 50 ; % initial velocity magnitude (m/s)
Vx0 = 41.315 ; % initial horizontal velocity (m/s)
Vy0 = 21.1309 ; % initial vertical velocity (m/s)
r = 0.03 ; % radius (m)
A = pi*(r)^2 ; % cross sectional area of projectile (m^2)
Cdrag = 0.80 ; % drag coefficient (unitless)
rho = 1.183 ; % air density (kg/m^3)
g = 9.81 ; % gravity (m/s^2)
%% Numerical Solution (With Drag)
t = 10 ;
dt = 0.01 ; % Time step (seconds)
Niter = floor(10/0.01) ; % total number of intervals (t/dt)
XxN(1) = Xx0 ;
XxN(2) = Xx0+(dt*Vx0) ;
XyN(1) = Xy0 ;
XyN(2) = Xy0+(dt*Vy0) ;
for i = 3:Niter
XxNow = XxN(i-1) ;
XxPrev = XxN(i-2) ;
XyNow = XyN(i-1) ;
XyPrev = XyN(i-2) ;
fx = @(XxNext)m*((XxNext-(2*XxNow)+XxPrev)/(dt^2)+(0.5*Cdrag*rho*A)...
*(sqrt(((XxNow-XxPrev/dt)^2)+((XyNow-XyPrev/dt)^2))))*(XxNext-XxPrev/2*dt) ;
fy = @(XyNext)m*((XyNext-(2*XyNow)+XyPrev)/(dt^2)+(0.5*Cdrag*rho*A)...
*(sqrt(((XxNow-XxPrev/dt)^2)+((XyNow-XxPrev/dt)^2))))*(XyNext-XyPrev/2*dt)+(m*g) ;
XxNext = fzero(fx,XxNow) ;
xxN(i) = XxNext ;
XyNext = fzero(fy,XyNow) ;
xyN(i) = XyNext ;
end

回答(1 个)

KSSV
KSSV 2020-5-22
There was a type error in updating XxN.....it was typed as xxN instead of XxN.....find the below corrected code:
close all
clc
%% Problem Parameters
m = 0.05 ; % mass (kg) = 50x10^-3
angle = 25 ; % initial angle (degrees)
th0 = angle*(pi/180) ; % initial angle (radians)
Xx0 = 0 ; % initial horizontal displacement (m)
Xy0 = 50 ; % initial vertical displacement (m)
V0 = 50 ; % initial velocity magnitude (m/s)
Vx0 = 41.315 ; % initial horizontal velocity (m/s)
Vy0 = 21.1309 ; % initial vertical velocity (m/s)
r = 0.03 ; % radius (m)
A = pi*(r)^2 ; % cross sectional area of projectile (m^2)
Cdrag = 0.80 ; % drag coefficient (unitless)
rho = 1.183 ; % air density (kg/m^3)
g = 9.81 ; % gravity (m/s^2)
%% Numerical Solution (With Drag)
t = 10 ;
dt = 0.01 ; % Time step (seconds)
Niter = floor(10/0.01) ; % total number of intervals (t/dt)
XxN = zeros(Niter,1) ;
XyN = zeros(Niter,1) ;
XxN(1) = Xx0 ;
XxN(2) = Xx0+(dt*Vx0) ;
XyN(1) = Xy0 ;
XyN(2) = Xy0+(dt*Vy0) ;
for i = 3:Niter
XxNow = XxN(i-1) ;
XxPrev = XxN(i-2) ;
XyNow = XyN(i-1) ;
XyPrev = XyN(i-2) ;
fx = @(XxNext)m*((XxNext-(2*XxNow)+XxPrev)/(dt^2)+(0.5*Cdrag*rho*A)...
*(sqrt(((XxNow-XxPrev/dt)^2)+((XyNow-XyPrev/dt)^2))))*(XxNext-XxPrev/2*dt) ;
fy = @(XyNext)m*((XyNext-(2*XyNow)+XyPrev)/(dt^2)+(0.5*Cdrag*rho*A)...
*(sqrt(((XxNow-XxPrev/dt)^2)+((XyNow-XxPrev/dt)^2))))*(XyNext-XyPrev/2*dt)+(m*g) ;
XxNext = fzero(fx,XxNow) ;
XxN(i) = XxNext ;
XyNext = fzero(fy,XyNow) ;
XyN(i) = XyNext ;
end
  7 个评论
KSSV
KSSV 2020-5-23
The code is working fine for me......Breakingpoint can be easily known...it will appear as a red dot on the left of the editor.

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