Adaptive Sliding Mode Control for Attitude Stabilization With Actuator Saturation
By Zhenglong Zhu, Yuanqing Xia, M. Fu. IEEE transactions on industrial electronics (1982. Print), 2011
382 citations recorded by the source corpus.
Subfields: Aerospace Engineering, Control and Systems Engineering
View Paper: https://www.semanticscholar.org/paper/527c46e10f392e963f926093bf1d4e65e336c511
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In Aerospace Engineering
In Control and Systems Engineering
Citations in the corpus
- Fault-Tolerant Tracking Control of Spacecraft with Attitude-Only Measurement Under Actuator Failures (2014, methodology): “In [49], a sliding-mode control law was synthesized for attitude stabilization with actuator saturation.”
- Adaptive Sliding Mode Control for Interval Type-2 Fuzzy Systems (2016, background): “By designing a sliding mode controller, the work in [57] investigated the attitude stabilization problem for a spacecraft system with inertia uncertainty and external disturbance.”
- Partial Integrated Missile Guidance and Control with Finite Time Convergence (2013, background): “However, if so, the control law can only guarantee the bounded motion around the sliding surface [12,33,34], which means convergence to the sliding surface is lost.”