Added a matlab test for earth rotation

release/4.3a0
djensen 2014-02-04 11:24:17 -05:00
parent 7049e83593
commit 5a8dab068e
1 changed files with 99 additions and 0 deletions

View File

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clc
clear all
close all
import gtsam.*;
deltaT = 0.1;
timeElapsed = 10;
times = 0:deltaT:timeElapsed;
%omega = [0;0;7.292115e-5]; % Earth Rotation
omega = [0;0;5*pi/10];
velocity = [0;0;0]; % initially not moving
accelFixed = [0;0.1;0.1]; % accelerate in the positive z-direction
initialPosition = [0; 1.05; 0]; % start along the positive x-axis
% Initial state
currentPoseFixedGT = Pose3(Rot3, Point3(initialPosition));
currentVelocityFixedGT = velocity;
currentPoseRotatingGT = currentPoseFixedGT;
currentPoseRotatingFrame = Pose3;
% Positions
positionsFixedGT = zeros(3, length(times)+1);
positionsRotatingGT = zeros(3, length(times)+1);
positionsFixedGT(:,1) = currentPoseFixedGT.translation.vector;
positionsRotatingGT(:,1) = currentPoseRotatingGT.translation.vector;
changePoseRotatingFrame = Pose3.Expmap([omega*deltaT; 0; 0; 0]);
poses(1).p = currentPoseRotatingFrame.translation.vector;
poses(1).R = currentPoseRotatingFrame.rotation.matrix;
h = figure(1);
i = 2;
for t = times
%% Create ground truth trajectory
% Update the pose and velocity
currentPositionFixedGT = Point3(currentPoseFixedGT.translation.vector ...
+ currentVelocityFixedGT * deltaT + 0.5 * accelFixed * deltaT * deltaT);
currentVelocityFixedGT = currentVelocityFixedGT + accelFixed * deltaT;
currentPoseFixedGT = Pose3(Rot3, currentPositionFixedGT);
% Rotate pose in fixed frame to get pose in rotating frame
currentPoseRotatingFrame = currentPoseRotatingFrame.compose(changePoseRotatingFrame);
currentPoseRotatingGT = currentPoseFixedGT.transform_to(currentPoseRotatingFrame);
% Store GT (ground truth) poses
positionsFixedGT(:,i) = currentPoseFixedGT.translation.vector;
positionsRotatingGT(:,i) = currentPoseRotatingGT.translation.vector;
poses(i).p = currentPoseRotatingFrame.translation.vector;
poses(i).R = currentPoseRotatingFrame.rotation.matrix;
% incremental graphing
figure(h)
plot_trajectory(poses(i),1, '-k', 'Rotating Frame',0.1,0.75,1)
hold on;
plot3(positionsFixedGT(1,:), positionsFixedGT(2,:), positionsFixedGT(3,:));
plot3(positionsRotatingGT(1,:), positionsRotatingGT(2,:), positionsRotatingGT(3,:), '-r');
plot3(positionsFixedGT(1,1), positionsFixedGT(2,1), positionsFixedGT(3,1), 'o');
plot3(positionsFixedGT(1,end), positionsFixedGT(2,end), positionsFixedGT(3,end), 'x');
plot3(positionsRotatingGT(1,1), positionsRotatingGT(2,1), positionsRotatingGT(3,1), 'or');
plot3(positionsRotatingGT(1,end), positionsRotatingGT(2,end), positionsRotatingGT(3,end), 'xr');
hold off;
xlabel('X axis')
ylabel('Y axis')
zlabel('Z axis')
axis equal
grid on;
pause(0.1);
i = i + 1;
end
figure
sphere
hold on;
plot3(positionsFixedGT(1,:), positionsFixedGT(2,:), positionsFixedGT(3,:));
plot3(positionsRotatingGT(1,:), positionsRotatingGT(2,:), positionsRotatingGT(3,:), '-r');
% beginning and end points of Fixed
plot3(positionsFixedGT(1,1), positionsFixedGT(2,1), positionsFixedGT(3,1), 'o');
plot3(positionsFixedGT(1,end), positionsFixedGT(2,end), positionsFixedGT(3,end), 'x');
% beginning and end points of Rotating
plot3(positionsRotatingGT(1,1), positionsRotatingGT(2,1), positionsRotatingGT(3,1), 'or');
plot3(positionsRotatingGT(1,end), positionsRotatingGT(2,end), positionsRotatingGT(3,end), 'xr');
xlabel('X axis')
ylabel('Y axis')
zlabel('Z axis')
axis equal
grid on;
hold off;