Hallo everyone, I'm trying to simulate a free fall-project, from the stratosphere (about 50 km) to the ground. So, in order to conclude an appropriate solution, drag must be put in consideration. I've allready found a proper solution for the Euler-method, but not for the ode45-method. Furthermore I need to put the [vector-]solutions of the acceleration (the differnecial) for every single calculation-step, in the velocity terms, I mean you could realize this one easy, by putting a while-slope in the code, that the steps would repeat itself until completion. But now to my issue, I've tried many approches with the ode45-method, but non of those have worked out.
Here my code:
function [a] = Test2 start=[0]; tspan=[0 100]; [t,A] = ode45(@Beschleunigung, tspan, start); %a(end+1) = - g + 1/(2*m)* c_w * A * rho(end)* (v(end))^2;
plot(t,A(:,1));end function dv = Beschleunigung(t, v) g = 9.81; m = 120; c_w = 0.28; A = 2.7; rho = 1.2041; dt = 0.5; hi = 40000; vi = 0; t = [0]; % Deklaration des Zeit-Arrays
h = [hi]; % Deklaration des Höhe-Arrays
v = [vi]; % Deklaration des Geschwindigkeits-Arrays
a = [0]; % Deklaration des Beschleunigungs-Arrays
dv = zeros(2,1); a=dv(1,end); dv(1,end+1) = g-(1/2*m)*c_w*A*rho*v^2; v(end+1)=v(end)+dv(1,end)*dt; h(end+1)=h(end)+v(end)*dt; t(end+1)=t(end)+dt; end
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