N=yaircraft(:,10);
E=yaircraft(:,11);
hp=yaircraft(:,12);
V=yaircraft(:,13);
time=taircraft(:,1);
Xdot=yaircraft(:,17);
Ydot=yaircraft(:,18);
R=yaircraft(:,9);

figure(1)
plot(EWP,NWP,'r+')
xlabel('Y-East (ft)')
ylabel('X-North (ft)')
hold on
plot(EWP,NWP,'r--')
%axis([0 44000 -44000 44000])
plot(E,N)
axis square
hold off
%hold off

figure(2)
subplot(411);
plot(time,V)

subplot(412);
plot(time,hp)
subplot(413);
plot(time,Xdot)
ylabel('Xdot')
subplot(414);
plot(time,Ydot)
ylabel('Ydot')
figure(3)
subplot(411);
plot(time,nextMat)
ylabel('next')
%plot(time,nextMat)
subplot(412);
plot(time,R)
ylabel('R')
subplot(413);
plot(time,deltaR)
ylabel('deltaR')
subplot(414);
plot(time,nextMat)
ylabel('next')


