Actuator failure compensation and attitude control for rigid satellite by adaptive control using quaternion feedback

DOI10.1016/J.JFRANKLIN.2013.08.028zbMath1293.93249OpenAlexW1995637782MaRDI QIDQ398367

Yuehua Cheng, Yajie Ma, Bin Jiang, Tao, Gang

Publication date: 15 August 2014

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

Full work available at URL: https://doi.org/10.1016/j.jfranklin.2013.08.028

zbMATH Keywords

adaptive controlattitude controlexternal disturbanceactuator failure compensationadaptive failure compensation controllerquaternion feedbackrigid satellite

Mathematics Subject Classification ID

Sensitivity (robustness) (93B35) Feedback control (93B52) Adaptive control/observation systems (93C40)

Related Items (9)

Global attitude stabilization of rigid spacecraft with unknown input delay ⋮ Adaptive integral sliding mode control for spacecraft attitude tracking with actuator uncertainty ⋮ Anti-disturbance fault-tolerant attitude control for satellites subject to multiple disturbances and actuator saturation ⋮ Finite-time attitude maneuvering and vibration suppression of flexible spacecraft ⋮ Integral Sliding Mode Fault-Tolerant Control for Spacecraft With Uncertainties and Saturation ⋮ On elliptic biquaternion matrices ⋮ Finite-time sliding mode attitude control for rigid spacecraft without angular velocity measurement ⋮ Third‐order sliding mode fault‐tolerant control for satellites based on iterative learning observer ⋮ A robust meta-heuristic adaptive Bi-CGSTAB algorithm to online estimation of a three DoF state–space model in the presence of disturbance and uncertainty

Cites Work

• Unnamed Item
• Fault tolerant control for a class of nonlinear systems with application to near space vehicle
• Mixed \(\mathcal H_2/\mathcal H_{\infty}\) approach to fault detection of discrete linear repetitive processes
• Adaptive nonlinear control without overparametrization
• Control of underactuated spacecraft with bounded inputs
• Sliding mode attitude tracking of rigid spacecraft with disturbances
• Autonomous impulsive rendezvous for spacecraft under orbital uncertainty and thruster faults
• Robust fault tolerant tracking controller design for a VTOL aircraft
• Robust attitude stabilization of spacecraft using nonlinear quaternion feedback
• Attitude Tracking and Disturbance Rejection of Rigid Spacecraft by Adaptive Control
• Inverse optimal adaptive control for attitude tracking of spacecraft
• Fault Accommodation for Nonlinear Dynamic Systems

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