Global Set Stabilization of the Spacecraft Attitude Control Problem Based on Quaternion

@inproceedings{Li2008GlobalSS,
  title={Global Set Stabilization of the Spacecraft Attitude Control Problem Based on Quaternion},
  author={Shihua Li and Shihong Li},
  year={2008}
}
In this paper, we develop a global set stabilization method for the attitude control problem of spacecraft system based on quaternion. The control law which uses both optimal control and finite-time control techniques can globally stabilize the attitude of spacecraft system to an equilibrium set. First for the kinematic subsystem, we design a virtual optimal angular velocity. Then for the dynamic subsystem, we design a finite-time control law which can force the angular velocity to track the… CONTINUE READING

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