Topology optimization method of satellite system
A satellite system and topology optimization technology, applied in the field of satellite system topology optimization
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[0170] Such as Figure 6 As shown, it is a system topology diagram of a satellite system. First, the system topology is not in the running state (Running=0), and the method of the present invention is used to determine the integrity key point.
[0171] Calculate each index value of each node, as shown in Table 3 below, and perform index screening by the method of maximum irrelevance.
[0172] Table 3 Each index value of each node
[0173]
Indicator 1
Indicator 2
Indicator 3
Indicator 4
Indicator 5
Indicator 6
Indicator 7
node 1
0.8000
0.9600
1.0000
0.0217
0.2099
92.0000
3.5333
node 2
0.9000
0.9900
1.0000
0.0217
0.2099
92.0000
3.5333
node 3
0.9000
0.9600
1.0000
0.0217
0.2099
92.0000
3.5333
node 4
0.9500
0.9900
4.0000
0.0313
0.6543
1216.0000
11.5167
node 5
0.8500
0.9700
2.0000
0.0333
0.6049
600.0000
9.35...
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