Performance of Gradient-Based Solutions versus Genetic Algorithms in the Correlation of Thermal Mathematical Models of Spacecrafts

Table 11

Temperature results (°C).

Node	Case 1	Case 2	Case 1	Case 2
1	36.27	36.27	25.69	25.69
2	28.53	28.53	29.38	29.89
3	30.13	30.13	25.51	26.62
4	20.00	20.00	20.00	20.00