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 Ding Qi 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

Citations

Publications citing this paper.
SHOWING 1-10 OF 27 CITATIONS

Asymptotic stabilization of quadrotor helicopter's attitude using an optimal hierarchical control technique

  • 2014 IEEE International Conference on Robotics and Biomimetics (ROBIO 2014)
  • 2014
VIEW 4 EXCERPTS
CITES METHODS
HIGHLY INFLUENCED

Attitude output feedback tracking control of satellites without angular velocity observers

  • IECON 2017 - 43rd Annual Conference of the IEEE Industrial Electronics Society
  • 2017
VIEW 1 EXCERPT
CITES METHODS

Fuzzy Adaptive Fault-Tolerant Output Feedback Attitude-Tracking Control of Rigid Spacecraft

  • IEEE Transactions on Systems, Man, and Cybernetics: Systems
  • 2017
VIEW 2 EXCERPTS
CITES BACKGROUND

Attitude consensus using quaternion-based controller composing augmented dynamic

  • 2014 IEEE 4th International Conference on System Engineering and Technology (ICSET)
  • 2014
VIEW 1 EXCERPT
CITES METHODS

Distributed attitude control for multiple spacecraft with communication delays

  • IEEE Transactions on Aerospace and Electronic Systems
  • 2014
VIEW 2 EXCERPTS
CITES METHODS & BACKGROUND

References

Publications referenced by this paper.
SHOWING 1-10 OF 18 REFERENCES

Similar Papers

Loading similar papers…