Ver las trayectorias

Moved las trayectorias si pensais
que los aviones van a chocar.

U = (5.50812917268506, 3.5600616617169996)
T = (-5.004461075743067, -6.529684446383383)
coefmont: (y(T) - y(U)) / (x(T) - x(U))
bmont: y(T) - coefmont * x(T)
t = 0.5 (slider from 0 to 300, step 0.1)
S = (5.543895223886391, -2.5380500681099964)
R = Point(yAxis)
coefdec: (y(S) - y(R)) / (x(S) - x(R))
bdec: y(S) - coefdec * x(S)
a = 1 (slider from 0 to 5, step 0.1)
A = (-0.014127590224525949, -0.0075108707522807405)
c = Circle(A, a)
d = Circle(A, a + 1.0)
e = Circle(A, a + 2.0)
f = Circle(A, a + 3.0)
g = Circle(A, a + 4.0)
b = Line(A, xAxis)
B, C = Intersect(g, b)
D = Rotate(C, t, A)
h = Segment(A, D)
E, F = Intersect(g, yAxis)
i = AngularBisector(C, A, E)
G, H = Intersect(g, i)
j = Line(E, xAxis)
k = Line(C, yAxis)
l = Line(B, yAxis)
m = Line(F, xAxis)
I = Intersect(k, j)
J = Intersect(j, l)
K = Intersect(m, l)
L = Intersect(m, k)
poly1, j_1, i_1, l_1, k_1 = Polygon(J, I, L, K)
O = (9.205516247725086, 3.6815052885711195)
Q = (11.776165411769577, 2.1581576358040144)
n = Line(R, S)
M: ((t - 50.0) / 50.0, coefdec * (t - 50.0) / 50.0 + bdec)
cli: round(Mod[t, 2.0])
p = Line(T, U)
N: ((t - 100.0) / 45.0, coefmont * (t - 100.0) / 45.0 + bmont)
q = Segment(E, F)
r = Segment(B, C)
P = Intersect(n, j_1)
V = Intersect(n, i_1)
W = Intersect(p, l_1)
Z = Intersect(p, i_1)
s = Segment(P, V)
a1 = Segment(W, Z)
o = false
c1 = Circle(U, 0.5)
d1 = Circle(S, 0.5)
b1 = Line(U, i_1)
e1 = Line(S, i_1)
A1, B1 = Intersect(c1, b1)
C1, D1 = Intersect(d1, e1)
u = Vector(U, A1)
v = Vector(U, B1)
w = Vector(S, C1)
z = Vector(S, D1)