Results of Short-Period Helicopter System Identification Using Output-Error and Hybrid Search-Gradient Optimization Algorithm

Table 1

AS355-F2 inertia and mass data.

Parameter	Data
Mass (kg)	2200
$I_y$ (kg$\mathrm{\hspace{0.17em}\hspace{0.17em}}·\mathrm{\hspace{0.17em}\hspace{0.17em}}$m^2)	1.1996e+004