Research Article
An Improved Feedforward-Robust Algorithm for Active Vibration Control of Helicopter Maneuver Flight
Table 1
Parameters of the beam structure.
| | Parameters | Data |
| | Mass (kg) | | | Density (kg/m3) | | | Modulus of elasticity (GPa) | | | Poisson’s ratio | 0.3 | | First natural frequency (Hz) | 8.2, 11.2, 16.7, 26.9, 33.2, 50.4, 56.9 |
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