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

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Figure 43. Weight Variation on Force Support.<br />

This first part of the analysis showed that the results are robust for most of the<br />

alternatives. The exception is related to the UAV and CGO aircraft systems, which<br />

showed some sensitivity to variations in the weights of Force Awareness and Force<br />

Mobility.<br />

Utility<br />

0.574<br />

0.000 0 100<br />

6.2 Hypothetical Scenarios<br />

Percent of Weight on Force<br />

Support<br />

The second part of the sensitivity analysis proposes two simple hypothetical<br />

scenarios to check if significant changes occur in the ranking of the alternatives. The<br />

hypothetical DM was asked to change the weights of the fundamental objectives,<br />

according to his assessment of the scenario in hand. A short description of the proposed<br />

scenarios can be found in Appendix 6.<br />

85<br />

Helicopter B (HLB)<br />

Cargo (CGO)<br />

Anti-submarine (ASW)<br />

Fighter (FTR)<br />

Helicopter A (HLA)<br />

Unmanned (UAV)

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