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

Table 4

Error values achieved with the GA for steady-state cases (°C).

	GA; Try 01	GA; Try 02	GA; Try 03	GA; Try 04	GA; Try 05	GA; Average
Hot case (°C)	0.190	0.216	0.237	0.392	0.301	0.267
Cold case (°C)	0.407	0.310	0.439	0.318	0.293	0.353