Discussion on: ``Adaptive variable structure maneuvering control and vibration reduction of three-axis stabilized flexible spacecraft

DOI10.1016/S0947-3580(06)70510-6zbMath1293.93152OpenAlexW4237905587MaRDI QIDQ2512082

Stefano Di Gennaro

Publication date: 7 August 2014

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

Full work available at URL: https://doi.org/10.1016/s0947-3580(06)70510-6

Mathematics Subject Classification ID

Sensitivity (robustness) (93B35) Feedback control (93B52) Nonlinear systems in control theory (93C10) Variable mass, rockets (70P05) Variable structure systems (93B12)

Cites Work

• Unnamed Item
• Distributed actuator control design for flexible beams
• Stabilization for continuum models of large space structures in large attitude maneuvers
• Exact nonlinear control of large angle rotational maneuvers
• Quaternion feedback for spacecraft large angle maneuvers
• Distributed piezoelectric-polymer active vibration control of a cantilever beam
• The attitude control problem
• Vibration Control Of Flexible Spacecraft Integrating A Momentum Exchange Controller And A Distributed Piezoelectric Actuator
• A unifying framework for the semiglobal stabilization of nonlinear uncertain systems via measurement feedback
• Input saturation and global stabilization of nonlinear systems via state and output feedback
• Robust attitude stabilization of spacecraft using nonlinear quaternion feedback
• Semiglobal stabilization of linear discrete-time systems subject to input saturation, via linear feedback-an ARE-based approach

This page was built for publication: Discussion on: ``Adaptive variable structure maneuvering control and vibration reduction of three-axis stabilized flexible spacecraft