Research Article
Observer Based Optimal Vibration Control of a Full Aircraft System Having Active Landing Gears and Biodynamic Pilot Model
Table 3
Comparison of peak values of acceleration responses for both controlled and uncontrolled cases.
| ā | Bump | Random | ā | Passive | Controller 2 | Controller 1 | Passive | Controller 2 | Controller 1 |
| | 0.5654 | 0.2290 | 0.1939 | 0.3860 | 0.4077 | 0.3017 | | 1.0303 | 0.2195 | 0.1782 | 2.4260 | 0.6801 | 0.4733 | | 0.6417 | 0.2766 | 0.3164 | 0.8143 | 0.3963 | 0.3406 | | 0.1874 | 0.0828 | 0.0667 | 0.6057 | 0.2958 | 0.2442 |
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