Attitude tracking control of a flexible spacecraft under angular velocity constraints

DOI10.1080/00207179.2017.1398841zbMath1417.93229OpenAlexW2765954248MaRDI QIDQ4967662

Laurent Burlion, Tarek Ahmed-Ali, Jean-Marc Biannic

Publication date: 3 July 2019

Published in: International Journal of Control (Search for Journal in Brave)

Full work available at URL: https://doi.org/10.1080/00207179.2017.1398841

zbMATH Keywords

spacecraftanti-windupconstrained controlinterval observersattitude stabilisationtime-domain constraint

Mathematics Subject Classification ID

Sensitivity (robustness) (93B35) Application models in control theory (93C95) Lyapunov and other classical stabilities (Lagrange, Poisson, (L^p, l^p), etc.) in control theory (93D05)

Cites Work

• A tutorial on modern anti-windup design
• Interval observers for linear time-invariant systems with disturbances
• Spacecraft attitude control using magnetic actuators
• Barrier Lyapunov functions for the control of output-constrained nonlinear systems
• Control systems with input and output constraints
• Output attitude tracking for flexible spacecraft
• Spacecraft attitude control using explicit model predictive control
• Structured adaptive attitude control of a satellite
• Nonlinear internal model based attitude tracking and disturbance rejection
• Spin-axis stabilisation of underactuated rigid spacecraft under sinusoidal disturbance
• Time-response shaping using output to input saturation transformation
• Unit Quaternion-Based Output Feedback for the Attitude Tracking Problem
• Attitude Tracking and Disturbance Rejection of Rigid Spacecraft by Adaptive Control
• Asymptotically Stable Interval Observers for Planar Systems With Complex Poles

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