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) = pqk·(1/r)^{2}·( (1/I_{c})·pq·k·(1/R)·)^{(1/2)}·(1/6)·t^{3}+( (1/I_{c})·pq·k·(1/R)·)^{(1/2)}·ht+h
d_{t}[x] = pqk·(1/r)^{2}·( (1/I_{c})·pq·k·(1/R)·)^{(1/2)}·(1/2)·t^{2}+( (1/I_{c})·pq·k·(1/R)·)^{(1/2)}·h
