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[Sample B: Approval/Signature Sheet] - George Mason University

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Utility<br />

0.560<br />

0.000 0 100<br />

Figure 42. Weight Variation on Force Mobility.<br />

Finally, small variations in the weight of Force Support do not show any<br />

significant change in the results of the sensitivity analysis. The utilities of HLA and UAV<br />

vary exactly the same with the variations of weight on Force Support. The variations in<br />

the marginal contribution yielded by HLA are caused by the variations in the utility of<br />

HLB, which has some of its main capabilities linked to the Force Support fundamental<br />

objective (see fig. 43).<br />

ACFT Force Sup.<br />

(14.79%)<br />

Percent of Weight on Force Mobility<br />

Table 8. Variation of Weight on Force Support.<br />

ACFT Force Sup.<br />

(24.79%)<br />

84<br />

Cargo (CGO)<br />

Helicopter A (HLA)<br />

Fighter (FTR)<br />

Helicopter B (HLB)<br />

Anti-submarine (ASW)<br />

Unmanned (UAV)<br />

ACFT Force Sup.<br />

(4.79%)<br />

FTR 0.488 FTR 0.432 FTR 0.546<br />

ASW 0.415 ASW 0.364 ASW 0.461<br />

UAV 0.272 UAV 0.242 UAV 0.306<br />

CGO 0.23 CGO 0.211 CGO 0.267<br />

HLA 0.167 HLA 0.098 HLA 0.227

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