Research Article
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) |
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