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The rotation around the 3 axis, we have denoted by Ω , the “right ascension of the ascending
node”, while the rotation around the intermediate 1 axis by i , the “inclination”. R 1 ( i )and R 3 ( Ω )
are orthonormal matrices such that ( 16.21 )holds.
cos Ω sin Ω 0
sin Ω cos i +cos Ω cos i sin i
+sin Ω sin i − cos Ω sin i cos i
R
3
×
3 .
R 1 ( i ) R 3 ( Ω )=
(16.21)
Accordingly, ( 16.22 ) is a representation of the placement vector x in the orthonormal bases
{
e 1 , e 2 , e 3 ,
O}
and
{
e 1 , e 2 , e 3 ,
O}
, respectively. Note that ( 16.23 )and( 16.24 )hold.
3
3
e i x i ,
e i x i =
x =
(16.22)
i =1
i =1
x 1 = x 1 cos Ω
x 2 sin Ω cos i + x 3 sin Ω sin i,
x 2 = x 1 sin Ω + x 2 cos Ω cos i
x 3 cos Ω sin i,
(16.23)
x 3 = x 2 sin i + x 3 cos i,
x 1 =+ x 1 cos Ω + x 2 sin Ω =: x ,
x 2 = −x 1 sin Ω cos i + x 2 cos Ω cos i + x 3 sin i =: y ,
(16.24)
x 3 =+ x 1 sin Ω sin i − x 2 cos Ω sin i + x 3 cos i =: z .
A 1 ,A 2
2
O
Corollary 16.1 (Intersection of
E
and
L
).
2
A 1 ,A 2
2
O
The intersection of the ellipsoid-of-revolution
E
and the central oblique plane
L
(two-
) is th e ellipse ( 16.25 ) of semi-major axis A 1 = A 1
dimensional linear manifold thr ough th e origin
O
and semi-minor axis A 2 = A 1 1
E 2 / 1
E 2 cos 2 i .
1
A 1 ,A 2
E
:=
1
:= x
E 2 cos 2 i ,A 1 >A 2 .
A 1 + y 2
x 2
E 2
2
=1 , A 1 = A 1 ,A 2 = A 1
R
|
1
(16.25)
A 2
End of Corollary.
Proof.
[( x 1 ) 2 +( x 2 ) 2 ] A 1 +( 16.23 )
(16.26)
[( x 1 ) 2 +( x 2 ) 2 ] A 1 = A 1 [ x 2 + y 2 cos 2 i + z 2 sin 2 i
2 y z sin i cos i ] ,
[( x 3 ) 2 ] A 2 +( 16.23 )
(16.27)
[( x 3 ) 2 ] A 2 = A 2 [ y 2 sin 2 i + z 2 cos 2 i ] ,
if x =0 , then
 
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