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.

	Bump			Random
	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