Autonomous Phase Control Combining EKF and Adaptive Neural Network for Remote Sensing Satellites

Table 3

Initial parameters of the system.

Parameters	Value
Thrust
Proportion coefficient
Satellite mass	=200 kg
Vacuum specific impulse	=2000
Moment of inertia
Initial attitude quaternion
Initial attitude angular velocity	(°/s)
Desired attitude quaternion
Desired attitude angular velocity	(°/s)