Using of H-Infinity Control Method in Attitude Control System of Rigid-Flexible Satellite

Table 1

Parameters.

Parameter	Description	Value
J0	Moments of inertia of the rigid body of the satellite	720 Kg⋅m^2
Jp	Moment of inertia of the panel	40 Kg⋅m^2
K	Constant elastic of the panels	320 Kg⋅rad^2/s^2
Kd	Dissipation constant	0,48 Kg⋅rad^2/s
L	Length of the panel	2 m
m	Mass of the satellite	200 kg