Design of the Microsatellite Attitude Control System Using the Mixed 𝐻₂/𝐻_∞ Method via LMI Optimization

Table 2

Actuator: reaction wheel.

Speed range (rpm)	±10000
Momentum capacity (N m s)	4
Reaction torque (N m)	150×10^−3
Mass (Kg)
Reaction wheel	<3.55
Motor driver	<1.2
Dimension (cm)	25×25×11