Altitude

Données

Altitude

Orbite

r = 6.367
C = Intersect(xAxis, yAxis)
c = Circle(C, r)
l1 = 48.9
l2 = 47.78
E: (-r, 0)
S_G = Rotate(E, -l1 °, C)
C_H = Rotate(E, -l2 °, C)
a = Segment(C_H, C)
b = Segment(C, S_G)
d = OrthogonalLine(C_H, a)
e = OrthogonalLine(S_G, b)
f = Segment(S_G, C_H)
H1 = 46.5
H2 = 36.3
B = Point(d)
B' = Rotate(B, H2 °, C_H)
g = Ray(C_H, B')
C_1 = Point(e)
C' = Rotate(C_1, H1 °, S_G)
h = Ray(S_G, C')
I_{S} = Intersect(h, g)
distanceISG = Distance(I_{S}, S_G)
TexteISG: "\overline{" + (Name[I_{S}]) + (Name[S_G]) + "} \, = \, " + distanceISG
distanceICH = Distance(I_{S}, C_H)
TexteICH: "\overline{" + (Name[I_{S}]) + (Name[C_H]) + "} \, = \, " + distanceICH
TexteC_{H}S = Distance(C_H, S_G)
C_HS: "\overline{" + (Name[C_H]) + (Name[S_G]) + "} \, = \, " + TexteC_{H}S
α = Angle(S_G, C_H, I_{S})
β = Angle(I_{S}, S_G, C_H)
γ = Angle(C_H, I_{S}, S_G)
k = Segment(I_{S}, C)
distanceCSG = Distance(C, S_G)
TexteCSG: "\overline{" + (Name[C]) + (Name[S_G]) + "} \, = \, " + distanceCSG
distanceSGI = Distance(S_G, I_{S})
δ = Angle(C, S_G, I_{S})
l = Distance(I_{S}, S_G)
text1: "\overline{" + (Name[I_{S}]) + (Name[S_G]) + "} \, = \, " + l
distanceIC = Distance(I_{S}, C)
TexteIC: "\overline{" + (Name[I_{S}]) + (Name[C]) + "} \, = \, " + distanceIC
i = false
j = false
ε = Angle(I_{S}, C, E)
m = Segment(E, C)
n = true