Adaptive attitude tracking control for rigid spacecraft with finite-time convergence

By Kunfeng Lu, Yuanqing Xia. at - Automatisierungstechnik, 2013

477 citations recorded by the source corpus.

Subfields: Aerospace Engineering, Control and Systems Engineering

View Paper: https://www.semanticscholar.org/paper/ac63698041d3cb2e29a2d34b70fc35523bf1c5a6

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. Yuanxin Li
2. Shaocheng Tong
3. Ding Wang
4. Derong Liu
5. Michael I. Friswell
6. Qinglei Hu
7. Boyan Jiang

In Control and Systems Engineering

1. Yuanxin Li
2. Shaocheng Tong
3. Ding Wang
4. Derong Liu
5. Tingwen Huang
6. Tao Tang
7. Junfeng Du
8. Jinying Li

Citations in the corpus

• Fixed-Time Attitude Control for Rigid Spacecraft With Actuator Saturation and Faults (2016, methodology): “Remark 2: The switching method (5) is inspired by [19] and [20] to avoid the singularity.”
• Event-Based Finite-Time Control for Nonlinear Multiagent Systems With Asymptotic Tracking (2023, background): “3197562 a higher convergence rate, superior tracking performance, and better robustness [15], [16], [17], [18], [19], [20].”
• Model-Free Optimal Tracking Control via Critic-Only Q-Learning (2016, background): “For many practical systems, such as hypersonic aircraft [35]–[37], spacecraft [38], [39], motion tracking [40], etc.”
• Iterative Learning Control with Extended State Observer for Telescope System (2015, background): “Introduction A high performance telescope system has attracted lots of attention, since it is widely used in space applications, such as space observer [1] and satellite surveillance [2].”