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 × 10^3	[kgm^2]
	100 × 10^3	[kgm^2]
	22 × 10^3	[kg]
	15	[kg]
	36	[kg]
	5.5	[kg]
	15	[kg]
	4.17	[kg]
	1.59 × 10^6	[N/m]
	1.59 × 10^6	[N/m]
	1.59 × 10^6	[N/m]
	6.73 × 10^5	[N/m]
	4.08 × 10^5	[N/m]
	4.08 × 10^5	[N/m]
	31 × 10^3	[N/m]
	49340	[N/m]
	2 × 10^4	[N/m]
	144 × 10^3	[N/m]
	1 × 10^4	[N/m]
	166990	[N/m]
	4066	[Ns/m]
	4066	[Ns/m]
	4066	[Ns/m]
	1.43 × 10^5	[Ns/m]
	6.25 × 10^5	[Ns/m]
	6.25 × 10^5	[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	—