Journal of Applied Mathematics / 2014 / Article / Tab 1

Research Article

Finite-Time Stabilization Control for a Rigid Spacecraft under Parameter Uncertainties

Table 1

Spacecraft model and controller parameters.

The project nameParameter

Spacecraft model parametersMoment of inertia  kg·m2
Initial position
Initial angular velocity  rad/s

Finite time controller ,   ,   ,   ,  
,   ,  

PID controller ,   ,