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fgdata/Aircraft-uiuc/Pioneer-TD/CDfade.dat
2000-10-22 21:05:31 +00:00

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2.1 KiB
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# Pioneer change in CD as function of alpha and elevator defection
-20
-7 0.0231
-6 0.0209
-5 0.0187
-4 0.0166
-3 0.0147
-2 0.0129
-1 0.0113
0 0.0098
1 0.0086
2 0.0074
3 0.0063
4 0.0053
5 0.0043
6 0.0031
7 0.0017
8 0.0001
9 -0.002
10 -0.0046
11 -0.0079
12 -0.012
13 -0.0171
14 -0.0234
15 -0.0311
16 -0.0403
17 -0.0543
-15
-7 0.0178
-6 0.0155
-5 0.0135
-4 0.0117
-3 0.0101
-2 0.0086
-1 0.0073
0 0.0061
1 0.005
2 0.004
3 0.003
4 0.002
5 0.001
6 0
7 -0.001
8 -0.002
9 -0.0031
10 -0.0042
11 -0.0054
12 -0.0067
13 -0.008
14 -0.0094
15 -0.0109
16 -0.0125
17 -0.0141
-10
-7 0.0111
-6 0.0095
-5 0.0081
-4 0.0069
-3 0.0057
-2 0.0047
-1 0.0038
0 0.003
1 0.0022
2 0.0015
3 0.0008
4 0.0001
5 -0.0006
6 -0.0013
7 -0.002
8 -0.0027
9 -0.0035
10 -0.0042
11 -0.005
12 -0.0058
13 -0.0067
14 -0.0075
15 -0.0084
16 -0.0093
17 -0.0102
-5
-7 0.0058
-6 0.005
-5 0.0043
-4 0.0037
-3 0.0031
-2 0.0025
-1 0.002
0 0.0016
1 0.0011
2 0.0007
3 0.0003
4 -0.0001
5 -0.0005
6 -0.0009
7 -0.0013
8 -0.0018
9 -0.0022
10 -0.0027
11 -0.0032
12 -0.0037
13 -0.0043
14 -0.0048
15 -0.0054
16 -0.006
17 -0.0066
0
-7 0
-6 0
-5 0
-4 0
-3 0
-2 0
-1 0
0 0
1 0
2 0
3 0
4 0
5 0
6 0
7 0
8 0
9 0
10 0
11 0
12 0
13 0
14 0
15 0
16 0
17 0
5
-7 -0.0028
-6 -0.0021
-5 -0.0015
-4 -0.001
-3 -0.0006
-2 -0.0003
-1 0
0 0.0003
1 0.0005
2 0.0007
3 0.001
4 0.0012
5 0.0014
6 0.0016
7 0.0018
8 0.002
9 0.0023
10 0.0025
11 0.0028
12 0.0031
13 0.0035
14 0.0038
15 0.0041
16 0.0045
17 0.0048
10
-7 -0.0053
-6 -0.0037
-5 -0.0024
-4 -0.0014
-3 -0.0005
-2 0.0002
-1 0.0008
0 0.0013
1 0.0018
2 0.0022
3 0.0026
4 0.003
5 0.0034
6 0.0039
7 0.0044
8 0.005
9 0.0056
10 0.0063
11 0.007
12 0.0078
13 0.0086
14 0.0095
15 0.0103
16 0.0111
17 0.0119
15
-7 -0.0063
-6 -0.0043
-5 -0.0025
-4 -0.001
-3 0.0002
-2 0.0013
-1 0.0022
0 0.0031
1 0.0039
2 0.0046
3 0.0053
4 0.006
5 0.0068
6 0.0076
7 0.0084
8 0.0093
9 0.0102
10 0.0112
11 0.0122
12 0.0133
13 0.0144
14 0.0155
15 0.0167
16 0.0177
17 0.0188
20
-7 -0.0029
-6 -0.0007
-5 0.0012
-4 0.0028
-3 0.0042
-2 0.0053
-1 0.0064
0 0.0074
1 0.0082
2 0.0091
3 0.0099
4 0.0108
5 0.0117
6 0.0126
7 0.0136
8 0.0147
9 0.0158
10 0.017
11 0.0182
12 0.0195
13 0.0209
14 0.0222
15 0.0236
16 0.025
17 0.0263