Robust adaptive sliding mode attitude maneuvering and vibration damping of three-axis-stabilized flexible spacecraft with actuator saturation limits

By Qinglei Hu. 2009

155 citations recorded by the source corpus.

Subfields: Aerospace Engineering, Control and Systems Engineering

View Paper: https://www.semanticscholar.org/paper/837bc7510f640b232d5e055f722ae455853d4694

How researchers see this paper

The researchers whose trusted networks rank it highest, strongest advocate first. Every researcher gets a different order.

In Aerospace Engineering

1. Qinglei Hu
2. Michael I. Friswell
3. Boyan Jiang
4. Yuanqing Xia
5. Zhenglong Zhu
6. M. Fu
7. Xu Jin

In Control and Systems Engineering

1. Qinglei Hu
2. Michael I. Friswell
3. Boyan Jiang
4. Yuanqing Xia
5. M. Fu
6. Zhenglong Zhu
7. Huijun Gao
8. Tongwen Chen

Citations in the corpus

• Fixed-Time Attitude Control for Rigid Spacecraft With Actuator Saturation and Faults (2016, background): “Hence, the problem of actuator saturation is another critical issue that needs to be tackled and many research results have been obtained [4]–[7].”
• Adaptive Sliding Mode Control for Attitude Stabilization With Actuator Saturation (2011, background): “Since 0 < χi(u2(t)) ≤ 1, according to the density property of a real number [16], there exists a constant δ that satisfies”