Output attitude tracking for flexible spacecraft

DOI10.1016/S0005-1098(02)00082-1zbMath1011.93522MaRDI QIDQ1858888

Yanyan Li

Publication date: 17 February 2003

Published in: Automatica (Search for Journal in Brave)

zbMATH Keywords

nonlinear controlflexible spacecraftoutput trackingdynamic control

Mathematics Subject Classification ID

Application models in control theory (93C95) Control of mechanical systems (70Q05)

Related Items (6)

Distributed attitude control for multiple flexible spacecraft under actuator failures and saturation ⋮ Robust attitude tracking control of flexible spacecraft for achieving globally asymptotic stability ⋮ Sliding mode attitude tracking of rigid spacecraft with disturbances ⋮ Adaptive-gain second-order sliding mode control of attitude tracking of flexible spacecraft ⋮ Active vibration isolation based on model reference adaptive control ⋮ Attitude tracking control of a flexible spacecraft under angular velocity constraints

Cites Work

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• Stabilization by smooth feedback of the angular velocity of a rigid body
• Functional analysis in modern applied mathematics
• Control of large flexible space structures
• Adaptive robust tracking for flexible spacecraft in presence of disturbances
• Spacecraft attitude control and stabilization: Applications of geometric control theory to rigid body models
• Exact nonlinear control of large angle rotational maneuvers
• The attitude control problem
• Global stabilization of flexible multibody spacecraft using quaternion-based nonlinear control law
• Robust attitude stabilization of spacecraft using nonlinear quaternion feedback
• Attitude control without angular velocity measurement: a passivity approach

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