Nonlinear Quadrocopter Attitude Control

[1]  Zdeněk Hurák,et al.  Advanced control of quadrotor using eigenaxis rotation , 2011, 2011 IEEE International Conference on Control Applications (CCA).

[2]  Ricardo G. Sanfelice,et al.  On quaternion-based attitude control and the unwinding phenomenon , 2011, Proceedings of the 2011 American Control Conference.

[3]  N. McClamroch,et al.  Rigid-Body Attitude Control , 2011, IEEE Control Systems.

[4]  Vijay Kumar,et al.  Minimum snap trajectory generation and control for quadrotors , 2011, 2011 IEEE International Conference on Robotics and Automation.

[5]  Ricardo G. Sanfelice,et al.  Quaternion-Based Hybrid Control for Robust Global Attitude Tracking , 2011, IEEE Transactions on Automatic Control.

[6]  Konrad Rudin,et al.  A Robust Attitude Controller and its Application to Quadrotor Helicopters , 2011 .

[7]  Abdelhamid Tayebi,et al.  Unit Quaternion-Based Output Feedback for the Attitude Tracking Problem , 2008, IEEE Transactions on Automatic Control.

[8]  Taeyoung Lee,et al.  Time optimal attitude control for a rigid body , 2007, 2008 American Control Conference.

[9]  Abdelhamid Tayebi,et al.  Attitude stabilization of a VTOL quadrotor aircraft , 2006, IEEE Transactions on Control Systems Technology.

[10]  Robert L. Grossman,et al.  Timed Automata , 1999, CAV.

[11]  B. Wie,et al.  Time-optimal three-axis reorientation of a rigid spacecraft , 1993 .

[12]  J. Wen,et al.  The attitude control problem , 1991 .

[13]  J. Stuelpnagel On the Parametrization of the Three-Dimensional Rotation Group , 1964 .