Mathematical Problems in Engineering / 2015 / Article / Tab 3

Research Article

Optimal Sizing of a Photovoltaic-Hydrogen Power System for HALE Aircraft by means of Particle Swarm Optimization

Table 3

PSO parameters.

ItemSymbolValue

Particles50
Maximum number of iterations300
Acceleration constants2
2
Initial inertia weight0.9
Final inertia weight0.4

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