Control of flexible spacecraft using dynamic inversion and µ-synthesis

DOI10.1177/1077546310369209zbMath1271.74342OpenAlexW2096456234MaRDI QIDQ2846397

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Publication date: 5 September 2013

Published in: Journal of Vibration and Control (Search for Journal in Brave)

Full work available at URL: https://doi.org/10.1177/1077546310369209

zbMATH Keywords

actuator saturationdynamic inversionnonlinear flexible spacecraft\(\mu \)-synthesis

Mathematics Subject Classification ID

Control, switches and devices (``smart materials) in solid mechanics (74M05) Vibrations in dynamical problems in solid mechanics (74H45) Control of mechanical systems (70Q05)

Related Items (3)

Chaotic attitude analysis of a satellite via Lyapunov exponents and its robust nonlinear control subject to disturbances and uncertainties ⋮ Nonlinear output feedback control of a flexible link using adaptive neural network: stability analysis ⋮ Nonlinear output feedback control of a flexible link using adaptive neural network: controller design

Cites Work

• Feedback linearization design of a ship steering autopilot with saturating and slew rate limiting actuator
• Design of nonlinear control laws for high-angle-of-attack flight
• Robust control law design for lateral-directional modes of an F-16/MATV using μ-synthesis and dynamic inversion
• Robust nonlinear ship course-keeping control byH? I/O linearization and?-synthesis
• Variable structure control and active vibration suppression of flexible spacecraft during attitude maneuver
• Adaptive robust attitude control of a flexible spacecraft

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