Staring Imaging Real-Time Optimal Control Based on Neural Network

Table 6

Other simulation parameters.

Parameter	Value
Satellite mass	1000 kg
Inertia tensor	, , , , , (kgm^2)
Star sensor constant error	3″
Star sensor random error ()	3″
Gyro constant error	0.15°/h
Gyro random error ()	0.15°/h
Reaction wheels constant error	0.01 nm
Reaction wheels random error ()	0.01 nm
External disturbance	Gravitational torque, aerodynamic torque, solar radiation torque and magnetic torque. (modeled according to ref. [23])
Initial Euler angle	Equal to the desired initial Euler angle for each ground target
Initial angular velocity	Equal to the desired initial angular velocity for each ground target