Research Article
Observer Based Optimal Vibration Control of a Full Aircraft System Having Active Landing Gears and Biodynamic Pilot Model
Table 1
The parameter values of the proposed full aircraft model and the numerical values of controlled variables coefficients.
| Symbol | Value | Units |
| | 130 | [kg] | | 260 | [kg] | | 260 | [kg] | | 65 × 103 | [kgm2] | | 100 × 103 | [kgm2] | | 22 × 103 | [kg] | | 15 | [kg] | | 36 | [kg] | | 5.5 | [kg] | | 15 | [kg] | | 4.17 | [kg] | | 1.59 × 106 | [N/m] | | 1.59 × 106 | [N/m] | | 1.59 × 106 | [N/m] | | 6.73 × 105 | [N/m] | | 4.08 × 105 | [N/m] | | 4.08 × 105 | [N/m] | | 31 × 103 | [N/m] | | 49340 | [N/m] | | 2 × 104 | [N/m] | | 144 × 103 | [N/m] | | 1 × 104 | [N/m] | | 166990 | [N/m] | | 4066 | [Ns/m] | | 4066 | [Ns/m] | | 4066 | [Ns/m] | | 1.43 × 105 | [Ns/m] | | 6.25 × 105 | [Ns/m] | | 6.25 × 105 | [Ns/m] | | 830 | [Ns/m] | | 2475 | [Ns/m] | | 330 | [Ns/m] | | 909.1 | [Ns/m] | | 200.00 | [Ns/m] | | 310.00 | [Ns/m] | | 7.76 | [m] | | 1.94 | [m] | | 3.8425 | [m] | | 3.8425 | [m] | | 7 | [m] | | 0.5 | [m] | | 450 | — | | 450 | — | | 150 | — | | 1 | — | | 50 | — | | 50 | — | | 50 | — |
|
|