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Table of Contents
Special Issues
Mathematical Problems in Engineering
/
2012
/
Article
/
Tab 3
/
Research Article
Semianalytic Integration of High-Altitude Orbits under Lunisolar Effects
Table 3
Inclination coefficients
𝑝
4
,
𝑗
,
𝑘
and
𝑝
5
,
𝑗
,
𝑘
; for brevity, we use the notation
𝛾
≡
(
1
±
𝑐
)
.
𝑗
𝑘
𝑝
4
,
𝑗
,
𝑘
𝑝
5
,
𝑗
+
1
,
𝑘
0
0
(
3
/
2
0
4
8
)
(
3
−
3
0
𝑐
2
+
3
5
𝑐
4
)
−
(
1
5
/
4
0
9
6
)
𝑠
(
1
−
1
4
𝑐
2
+
2
1
𝑐
4
)
±
1
−
(
1
5
/
5
1
2
)
𝑠
𝑐
(
3
−
7
𝑐
2
)
−
(
1
5
/
8
1
9
2
)
𝛾
(
1
±
2
8
𝑐
−
4
2
𝑐
2
∓
8
4
𝑐
3
+
1
0
5
𝑐
4
)
±
2
−
(
1
5
/
1
0
2
4
)
𝑠
2
(
1
−
7
𝑐
2
)
∓
(
1
0
5
/
4
0
9
6
)
𝑠
𝛾
(
1
∓
3
𝑐
−
9
𝑐
2
±
1
5
𝑐
3
)
±
3
(
3
5
/
5
1
2
)
𝑠
3
𝑐
(
3
5
/
1
6
3
8
4
)
𝑠
2
𝛾
(
1
±
6
𝑐
−
1
5
𝑐
2
)
±
4
(
1
0
5
/
4
0
9
6
)
𝑠
4
±
(
3
1
5
/
3
2
7
6
8
)
𝑠
3
𝛾
(
1
∓
5
𝑐
)
±
5
−
(
6
3
/
1
6
3
8
4
)
𝑠
4
𝛾
2
0
−
(
1
0
5
/
5
1
2
)
𝑠
2
(
1
−
7
𝑐
2
)
(
2
4
5
/
8
1
9
2
)
𝑠
3
(
1
−
9
𝑐
2
)
±
1
±
(
1
0
5
/
2
5
6
)
𝑠
𝛾
(
1
±
7
𝑐
−
1
4
𝑐
2
)
(
7
3
5
/
1
6
3
8
4
)
𝑠
2
𝛾
(
1
±
6
𝑐
−
1
5
𝑐
2
)
±
2
(
1
0
5
/
2
5
6
)
𝛾
2
(
1
∓
7
𝑐
+
7
𝑐
2
)
±
(
7
3
5
/
8
1
9
2
)
𝑠
𝛾
2
(
1
∓
1
2
𝑐
+
1
5
𝑐
2
)
±
3
∓
(
2
4
5
/
2
5
6
)
𝑠
𝛾
2
(
1
∓
2
𝑐
)
−
(
2
4
5
/
9
8
3
0
4
)
𝛾
3
(
1
3
∓
5
4
𝑐
+
4
5
𝑐
2
)
±
4
(
7
3
5
/
1
0
2
4
)
𝑠
2
𝛾
2
±
(
2
2
0
5
/
6
5
5
3
6
)
𝑠
𝛾
3
(
3
∓
5
𝑐
)
±
5
−
(
4
4
1
/
3
2
7
6
8
)
𝑠
2
𝛾
3
4
0
(
2
2
0
5
/
2
0
4
8
)
𝑠
4
−
(
6
6
1
5
/
8
1
9
2
)
𝑠
5
±
1
∓
(
2
2
0
5
/
5
1
2
)
𝑠
3
𝛾
−
(
3
3
0
7
5
/
1
6
3
8
4
)
𝑠
4
𝛾
±
2
(
2
2
0
5
/
1
0
2
4
)
𝑠
2
𝛾
2
±
(
3
3
0
7
5
/
8
1
9
2
)
𝑠
3
𝛾
2
±
3
∓
(
7
3
5
/
5
1
2
)
𝑠
𝛾
3
−
(
1
1
0
2
5
/
3
2
7
6
8
)
𝑠
2
𝛾
3
±
4
(
2
2
0
5
/
4
0
9
6
)
𝛾
4
±
(
3
3
0
7
5
/
6
5
5
3
6
)
𝑠
𝛾
4
±
5
−
(
1
3
2
3
/
3
2
7
6
8
)
𝛾
5
