mbs = input ('Mass of the bottom strut ');
xd = input ('Position of the plate after which the system is self deployable');
k = input ('Stiffness of the spring ');
jj =input ('The layer to which the spring belongs ');
dely = input ('The minimum deflection of the spring ');


N= LL/L;
c= 3 (N + 1);
h= (2 L A2) .5;
wp= mc 9.81;
wts= mts 9.81;
ws= (mts+mbs) 9.81;


%Constants:
x (1)= 0;
a (1)= 0;
t(1) 0;
v (1)=0;


% Initial conditions:
x (2) = xd;
a (2) = ((((( 6 k (h (((x(2) ^2)+(L A2)) A.5) + dely)* (cos ((atan (L/x(2))))))) (3 *
wp *jj ) -( 6 ws (jj 1 )))- ( 6 wts .5 (sin(( ( 2 atan (L/x(2))))))))/ ((3 mc *
jj ) + ( 6 (mbs + mts) (jj 1))));
t(2)=0.0001;
av(2)= a(2)/ 2;
v(2)=av (2) *t(2);
T(1)= 0;
T(2)= 0;


for i= 3 :(( (L-xd )/.01)+1)