Research Article

The Reduction of Modal Sensor Channels through a Pareto Chart Methodology

Table 3

Summary of natural frequencies.

Base95%90%75%Description

12.412.412.412.4Mode 1 wing bending
17.317.517.517.5Tail torsion, antisymmetric wingtip bend
20.820.820.821.0Wingtip, wing, tail, HS, VS torsion, and wingtip bend
26.726.026.025.9Wing torsion, slight HS bend
28.928.228.128.1Symmetric wing torsion
30.230.830.830.7Antisymmetric wingtip bend, tail wag
33.836.536.1—HS, VS torsion
39.939.739.839.8HS bend/torsion, mode 2 wing bend, and VS torsion
45.044.944.944.7Mode 2 wing bend, HS bend/torsion, and VS torsion
51.451.051.750.6Wing torsion, HS bend/torsion
63.761.162.964.1Antisymmetric wing torsion, HS bend, and fuselage bend
72.373.372.071.9Mode 2 wing bend/torsion opposite, HS torsion
74.475.975.975.8HS torsion, mode 2 wing bend and torsion