Research Article
The Reduction of Modal Sensor Channels through a Pareto Chart Methodology
Table 3
Summary of natural frequencies.
| Base | 95% | 90% | 75% | Description |
| 12.4 | 12.4 | 12.4 | 12.4 | Mode 1 wing bending | 17.3 | 17.5 | 17.5 | 17.5 | Tail torsion, antisymmetric wingtip bend | 20.8 | 20.8 | 20.8 | 21.0 | Wingtip, wing, tail, HS, VS torsion, and wingtip bend | 26.7 | 26.0 | 26.0 | 25.9 | Wing torsion, slight HS bend | 28.9 | 28.2 | 28.1 | 28.1 | Symmetric wing torsion | 30.2 | 30.8 | 30.8 | 30.7 | Antisymmetric wingtip bend, tail wag | 33.8 | 36.5 | 36.1 | ā | HS, VS torsion | 39.9 | 39.7 | 39.8 | 39.8 | HS bend/torsion, mode 2 wing bend, and VS torsion | 45.0 | 44.9 | 44.9 | 44.7 | Mode 2 wing bend, HS bend/torsion, and VS torsion | 51.4 | 51.0 | 51.7 | 50.6 | Wing torsion, HS bend/torsion | 63.7 | 61.1 | 62.9 | 64.1 | Antisymmetric wing torsion, HS bend, and fuselage bend | 72.3 | 73.3 | 72.0 | 71.9 | Mode 2 wing bend/torsion opposite, HS torsion | 74.4 | 75.9 | 75.9 | 75.8 | HS torsion, mode 2 wing bend and torsion |
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