Finite-time output feedback attitude control for rigid spacecraft under control input saturation

DOI10.1016/j.jfranklin.2016.08.013zbMath1349.93174OpenAlexW2509470969MaRDI QIDQ344632

An-Min Zou, Krishna Dev Kumar, Anton H. J. de Ruiter

Publication date: 24 November 2016

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

Full work available at URL: https://doi.org/10.1016/j.jfranklin.2016.08.013

zbMATH Keywords

observerstabilizing controlinput saturationfinite-time stabilityoutput feedback attitude controlquaternion-based attitude representationrigid spacecraft subject

Mathematics Subject Classification ID

Feedback control (93B52) Stabilization of systems by feedback (93D15) Observability (93B07) Control/observation systems governed by ordinary differential equations (93C15)

Related Items (10)

Fixed-time attitude tracking control for rigid spacecraft ⋮ Super-twisting observer-based sliding mode control with fuzzy variable gains and its applications to fully-actuated hexarotors ⋮ Predictive motion control for autonomous capture of a tumbling target with a space manipulator ⋮ Finite-time spacecraft attitude control under input magnitude and rate saturation ⋮ Finite-time path following control for small-scale fixed-wing UAVs under wind disturbances ⋮ Adaptive sliding mode control for uncertain Euler-Lagrange systems with input saturation ⋮ Adaptive fixed-time relative position tracking and attitude synchronization control for non-cooperative target spacecraft fly-around mission ⋮ Distributed fixed-time attitude coordinated tracking for multiple rigid spacecraft via a novel integral sliding mode approach ⋮ Predefined-time control for free-floating space robots in task space ⋮ Finite-time attitude control for rigid spacecraft subject to actuator saturation

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