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Shock and Vibration
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Shock and Vibration
/
2016
/
Article
/
Tab 2
/
Research Article
Observer Based Optimal Vibration Control of a Full Aircraft System Having Active Landing Gears and Biodynamic Pilot Model
Table 2
Road roughness and standard deviation [
22
].
Road class
σ
(10
−3
m)
(10
−6
m
3
),
(rad/m)
A (very good)
2
1
0.127
B (good)
4
4
0.127
C (average)
8
16
0.127
D (poor)
16
64
0.127
E (very poor)
32
256
0.127