- #1
petra
- 8
- 0
I have question for you,How calculate closest distance between two
ellipse in space.
orbit first : r = (p1)/(1+epsilon1*cos(theta1))
second orbit : r = (p2)/(1+epsilon2*cos(theta2))
the relation between two ellipse is some euler angles call them
first angle :a1
second angle :b1 (these three euler angles)
third angle :c1
(taking in account they have same focus :the sun)
? symbolic solution for this problem
? how solve this with approximation techniques.
what when orbit is not closed:hyperbole,parabole
ellipse in space.
orbit first : r = (p1)/(1+epsilon1*cos(theta1))
second orbit : r = (p2)/(1+epsilon2*cos(theta2))
the relation between two ellipse is some euler angles call them
first angle :a1
second angle :b1 (these three euler angles)
third angle :c1
(taking in account they have same focus :the sun)
? symbolic solution for this problem
? how solve this with approximation techniques.
what when orbit is not closed:hyperbole,parabole