Research Article

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

Table 8

GLs values for case 1 and case 2 [W/°C].

Parameter

Case 1 [W/°C]8.006.005.004.008.003.00
Case 2 [W/°C]6.007.005.578.006.942.97