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International Journal of Aerospace Engineering
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International Journal of Aerospace Engineering
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2017
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Article
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Tab 3
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Research Article
Performance of Gradient-Based Solutions versus Genetic Algorithms in the Correlation of Thermal Mathematical Models of Spacecrafts
Table 3
Error values achieved with Powell’s algorithms for steady-state cases (°C).
TOLMIN
NEWUOA
BOBYQA
LINCOA
Hot case (°C)
0.000
0.000
0.000
0.000
Cold case (°C)
0.351
0.000
0.442
0.351