Finite‐time constrained attitude regulation for spacecraft formation with disturbances on SO(3)$$ SO(3) $$
DOI10.1002/rnc.6620OpenAlexW4322008834MaRDI QIDQ6190416
Xiaofeng Zong, Renfu Li, Shengjie Zhu, Yuanyuan Zhang
Publication date: 6 February 2024
Published in: International Journal of Robust and Nonlinear Control (Search for Journal in Brave)
Full work available at URL: https://doi.org/10.1002/rnc.6620
communication delayfinite-time\(SO(3)\)artificial potential functionattitude constraintsnonsingular fast terminal sliding manifold
Sensitivity (robustness) (93B35) Perturbations in control/observation systems (93C73) Variable structure systems (93B12) Orbital mechanics (70M20) Finite-time stability (93D40)
Cites Work
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- Chattering Analysis
- Controller Class for Rigid Body Tracking on $\mathsf {SO}(3)$
- Delay Tolerance for Stable Stochastic Systems and Extensions
- Continuous adaptive-gain finite-time control for rigid body attitude dynamics on SO(3)
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