A simple saturated control framework for spacecraft with bounded disturbances

DOI10.1002/rnc.3303zbMath1332.93168OpenAlexW1937879376MaRDI QIDQ2792781

Hu Jinchang, Zhang Honghua

Publication date: 14 March 2016

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.3303

zbMATH Keywords

spacecraftsaturated controlattitude controlhigh-gain feedback controlprojection adaptive control

Mathematics Subject Classification ID

Nonlinear systems in control theory (93C10) Adaptive control/observation systems (93C40) Variable mass, rockets (70P05) Control/observation systems governed by ordinary differential equations (93C15)

Related Items (4)

Guaranteed cost control of rigid‐body attitude systems under control saturation ⋮ Robust adaptive control for spacecraft attitude synchronization subject to external disturbances: A performance adjustable event‐triggered mechanism ⋮ Attitude tracking of rigid spacecraft with actuator saturation and fault based on a compound control ⋮ Output feedback control for asymptotic stabilization of spacecraft with input saturation

Cites Work

• Control of underactuated spacecraft with bounded inputs
• On the stability and stabilization of quaternion equilibria of rigid bodies
• The attitude control problem
• Lyapunov Optimal Saturated Control for Nonlinear Systems
• Smooth sliding-mode control for spacecraft attitude tracking maneuvers
• Attitude control without angular velocity measurement: a passivity approach
• Unit Quaternion-Based Output Feedback for the Attitude Tracking Problem

This page was built for publication: A simple saturated control framework for spacecraft with bounded disturbances