To create a script that plots the trajectory of the geodesic equation in Matlab, we can follow these steps:
- Define the geodesic equation that we want to solve. This may depend on the specific problem we are interested in, but a general form for the geodesic equation in curved spacetime is:
This function calculates the second derivative of a four-vector x wrt proper time tau, given the metric tensor gamma.
- Choose the initial conditions for the particle. For example, we may set the initial position to [0;0;0] and the initial 4-velocity to [1;0;0;0]. We also need to specify the range of proper times over which we want to solve the geodesic equation.
- Choose the metric tensor for the spacetime we are interested in. For example, we may use the Schwarzschild metric for a non-rotating black hole:
This defines a function gamma
that takes a radial coordinate r
and returns the 4x4 metric tensor evaluated at that point. Note that we have set units where c=G=1.
- Solve the geodesic equation using Matlab's ODE solver
ode45
. This will give us the trajectory of the particle as a function of proper time.
- Plot the trajectory of the particle using Matlab's
plot3
function.
Putting these steps together, we obtain the following Matlab script:
% Define the geodesic equation
function d2x = geodesic_equation(t,x,gamma)
dtau = sqrt(gamma(x(1:3),x(1:3))*x(4:end)'*x(4:end)); % proper time interval
G = gamma(x(1:3),:);
d2x = [x(4:end);...
-(1/2)*sum(sum(inv(G).*reshape(sum(reshape(permute(sum(bsxfun(@times,G,reshape(x(4:end),1,1,[]))),2),[],3),size(G,1),size(G,2)),3).*reshape(bsxfun(@times,G(:,:,find(size(G,3)==size(G,2))),x(4:end)'),[],1,size(G,2)),2),1)/dtau^2];
% Set the initial conditions and range of proper time
x0 = [0;0;0;1;0;0;0];
tau_span = [0 10];
% Define the metric tensor
M = 1;
gamma = @(r) [-(1-2*M./r) zeros(1,3);...
zeros(3,1) eye(3)*(1-2*M./r)];
% Solve the geodesic equation
options = odeset('RelTol',1e-12,'AbsTol',1e-15);
sol = ode45(@(t,x) geodesic_equation(t,x,gamma), tau_span, x0, options);
% Plot the trajectory
x = sol.y(1:3,:);
plot3(x(1,:),x(2,:),x(3,:));
xlabel('x'); ylabel('y'); zlabel('z');
This script defines the geodesic equation, sets the initial conditions and spacetime metric, solves the geodesic equation using ode45
, and plots the resulting trajectory. Note that this is just one example of how to do this - the specific form of the geodesic equation will depend on the problem at hand, and the metric tensor may need to be adjusted accordingly.