Autonomous spacecraft rendezvous with finite time convergence

DOI10.1016/j.jfranklin.2015.08.008zbMath1395.93149OpenAlexW1666603596MaRDI QIDQ1660725

Defu Lin, Jiang Wang, Shaoming He

Publication date: 16 August 2018

Published in: Journal of the Franklin Institute (Search for Journal in Brave)

Full work available at URL: https://doi.org/10.1016/j.jfranklin.2015.08.008

zbMATH Keywords

nonsingular terminal sliding mode controlfinite time convergenceautonomous spacecraft rendezvous

Mathematics Subject Classification ID

Control/observation systems with incomplete information (93C41) Application models in control theory (93C95) Discrete-time control/observation systems (93C55) Observability (93B07) Variable structure systems (93B12)

Related Items (6)

Output feedback robust \(H_\infty\) control for spacecraft rendezvous system subject to input saturation: A gain scheduled approach ⋮ Adaptive fixed-time relative position tracking and attitude synchronization control for non-cooperative target spacecraft fly-around mission ⋮ Adaptive fuzzy finite-time control for spacecraft formation with communication delays and changing topologies ⋮ Distributed fixed-time attitude coordinated tracking for multiple rigid spacecraft via a novel integral sliding mode approach ⋮ Adaptive neural finite-time control for space circumnavigation mission with uncertain input constraints ⋮ Robust finite-time trajectory tracking control of wheeled mobile robots with parametric uncertainties and disturbances

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