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1
( q 1 b 1 + l 1 ) 3 ×
α 2 =
(16.72)
× s 2 ( q 1 b 1
l 1 )( q 1 b 1 + l 1 )+ s 1 ( q 1 b 2 + q 2 b 1 )(3 l 1
q 1 b 1 ) q 1 b 1
−l 1 l 2 (3 q 1 b 1 − l 1 ) ,
1
( q 1 b 1 + l 1 ) 3 ×
β 2 =
× 2 q 1 b 1 l 1 ( q 1 b 1 + l 1 ) s 2 + s 1 ( q 1 b 2 + q 2 b 1 )(
3 q 1 b 1 + l 1 ) l 1
3 l 1 + q 1 b 1 ) q 1 b 1 l 1 .
+(
End of Proof.
Equation ( 16.51 ), which represent locally the oblique Mercator projection, reduce (i) to the
equations of the standard Mercator projection of
2
A 1 ,A 2
E
for zero inclination, see Box 16.6 , or (ii)
2
A 1 ,A 2
for 90 inclination, see Box 16.7 ,
to the equations of the transverse Mercator projection of
E
2
or (iii) to the equations of the oblique Mercator projection of
S
r for zero relative eccentricity
E = 0, compare with Box 16.1 presented already before.
2
A 1 ,A 2
Box 16.6 (The equations of the standard Mercator projection of
E
for zero inclination).
i =0
(16.73)
E =0 , A 1 = A 1 , A 2 = A 1 ,
tan( L
Ω )=tan α
(16.74)
α = L
Ω,
tan B =0
(16.75)
j =1 , 2 ,...,
s 1 ( α )= A 1 = a, s 2 ( α )=0 ,s 3 ( α )=0 ,....,
b j =0
(16.76)
α 1 =0 2 =0 1 = s 1 = a, β 2 =0
(16.77)
Δx = aΔl, Δy = aΔq = αq 1 Δb + αq 2 Δb 2 +O 3 .
2
A 1 ,A 2
for 90 inclination).
Box 16.7 (The equations of the transverse Mercator projection of
E
i = π/ 2
(16.78)
A 2 = A 1 1
E = E, A 1 = A 1 ,
E 2 ,
 
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