Unit Quaternion-Based Output Feedback for the Attitude Tracking Problem

By Abdelhamid Tayebi. IEEE Transactions on Automatic Control, 2008

329 citations recorded by the source corpus.

Subfields: Control and Systems Engineering

View Paper: https://www.semanticscholar.org/paper/7f1b0c1438ee7ed936a085f22aef3e9865d7dbef

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In Control and Systems Engineering

1. Qinglei Hu
2. Yuanqing Xia
3. M. Fu
4. Zhenglong Zhu
5. Bing Xiao
6. Youmin Zhang
7. Xing Huo
8. Changbin Yu

Citations in the corpus

• Fault-Tolerant Tracking Control of Spacecraft with Attitude-Only Measurement Under Actuator Failures (2014, methodology): “Based on comparisons in Tables 2–4, it can be seen that, whether faults occur or not, the proposed control approach provides better performance than the controllers presented in [18].”
• Quaternion-Based Hybrid Control for Robust Global Attitude Tracking (2011, unknown): “The following discussion is of independent interest when quaternion filters are used (as in [20], [23], as well as in thi s paper) and also applies to designing a torque feedback, whic h we consider in the sequel.”
• Attitude Tracking of Rigid Spacecraft With Bounded Disturbances (2011, background): “In [6], the authors provide a solution to the attitude tracking problem by introducing a unit-quaternion auxiliary system which has the same structure as the actual unit-quaternion attitude model.”
• Adaptive Sliding Mode Control for Attitude Stabilization With Actuator Saturation (2011, background): “In [9], the authors provide a solution to the attitude tracking problem by introducing a unit-quaternion auxiliary system which has the same structure as the actual unit-quaternion attitude model.”
• The geometric structure of unit dual quaternion with application in kinematic control (2012, methodology): “In many existing literature concerning the designing of controllers and observers for systems on SO(3), instead of using the actual logarithm of unit quaternion, an approximate function that is quick and easy to compute algebraically is adopted [17–19].”
• Attitude Synchronization of a Group of Spacecraft Without Velocity Measurements (2009, background): “In this context, the authors in [13] present a local passivity based control law for multi-spacecraft attitude alignment without velocity measurements, assuming a ring communication topology.”
• Attitude stabilization of rigid spacecraft with finite‐time convergence (2011, background): “In [16], the authors provide a solution to the attitude tracking problem by introducing a unit-quaternion auxiliary system which has the same structure as the actual unit-quaternion attitude model.”