mecánica-lunar

Principio: [ orbital de cuerpo celeste ]

I_{c}·d_{t}[w]^{2} = pq·k·(1/R)

Ley

Órbita lunar:

B(d_{t}[w]) = qk·(1/r)^{2}·( (1/I_{c})·pq·k·(1/R) )^{(1/2)}

Alunizar:

E(w) = qk·(1/r)^{2}·( (1/I_{c})·pq·k·(1/R) )^{(1/2)}·t

Ley:

x(t) = (1/m)·pqk·(1/r)^{2}·( (1/I_{c})·pq·k·(1/R) )^{(1/2)}·(1/6)·t^{3}+...

... (-1)·( (1/I_{c})·pq·k·(1/R) )^{(1/2)}·ht+h

d_{t}[x] = (1/m)·pqk·(1/r)^{2}·( (1/I_{c})·pq·k·(1/R) )^{(1/2)}·(1/2)·t^{2}+...

... (-1)·( (1/I_{c})·pq·k·(1/R) )^{(1/2)}·h

d_{t}[x(t_{k})] = 0 <==> t_{k} = ( h·( (2m)/(pqk) )·r^{2} )^{(1/2)}

x(t_{k}) = 0 <==> h = ( ( (1/I_{c})·pq·k·(1/R) )·(2/3)·( ( (2m)/(pqk) )·r^{2} ) )^{(-1)}