Mathematical Problems in Engineering / 2015 / Article / Tab 4

Research Article

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

Table 4

Cases of study results.

AircraftPPVS/kWPSS/kWhPURFC/kWMASS/kgEFFS/%

PathfinderMean5.3724.4911.51191.0146.82
StDev
(CV)
0.25
(4.6%)
3.90
(15.9%)
1.50
(13.0%)
5.16
(2.7%)
1.05
(2.2%)
Min5.2022.928.38187.9244.55
Max5.9735.1812.22205.3647.60

Pathfinder plusMean6.0432.3615.01224.0947.81
StDev
(CV)
0.33
(5.4%)
6.04
(18.7%)
0.95
(6.3%)
7.69
(3.4%)
0.46
(1.0%)
Min5.8028.8812.40217.7746.90
Max6.7044.3315.40238.6648.28

Helios HP01Mean18.3188.8833.58589.9145.82
StDev
(CV)
0.80
(4.4%)
11.19
(12.6%)
4.01
(12.0%)
14.89
(2.5%)
0.92
(2.0%)
Min17.1073.8124.35565.6044.22
Max20.01104.4436.28608.0946.80

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