Robust controllers design with finite time convergence for rigid spacecraft attitude tracking control

By Erdong Jin, Zhao-wei Sun. 2008

225 citations recorded by the source corpus.

Subfields: Control and Systems Engineering

View Paper: https://www.semanticscholar.org/paper/3850e60393c83bb51beb7fd299d51abeee77f1ac

How researchers see this paper

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

In Control and Systems Engineering

1. Shihua Li
2. Haibo Du
3. Yuanqing Xia
4. Chunjiang Qian
5. Jianying Wang
6. Ming Liu
7. M. Fu
8. Zhenglong Zhu

Citations in the corpus

• Finite-Time Control for Spacecraft Formation with Dual-Number-Based Description (2012, methodology): “Lemma 3 [21]: If k 2 0; 1 , then the following inequality holds Xn”
• Attitude stabilization of rigid spacecraft with finite‐time convergence (2011, background): “In [20], two robust controllers based on quaternion feedback are proposed to achieve the attitude tracking of a rigid spacecraft in finite time.”
• Finite-Time Attitude Tracking Control of Spacecraft With Application to Attitude Synchronization (2011, methodology): “Different from [15], there is no singularity problem in our control law, since here we use another kind of finite-time control technique, i.”
• Adaptive attitude tracking control for rigid spacecraft with finite-time convergence (2013, background): “There are a few finite-time control results based on TSM or NTSM for spacecraft systems (Jin & Sun, 2008; Li, Wang, & Fei, 2011).”