Control Allocation for Spacecraft Under Actuator Faults
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Beschreibung
This book provides a systematical and comprehensive description of some facets of modeling, designing, analyzing and exploring the control allocation and fault-tolerant control problems for over-actuated spacecraft attitude control system under actuator failures, system uncertainties and disturbances. The book intends to provide a unified platform for understanding and applicability of the fault-tolerant attitude control and control allocation for different purposes in aerospace engineering and some related fields. And it is particularly suited for readers who are interested to learn solutions in spacecraft attitude control system design and related engineering applications.
This book provides a systematical and comprehensive description of some facets of modeling, designing, analyzing and exploring the control allocation and fault-tolerant control problems for over-actuated spacecraft attitude control system under actuator failures, system uncertainties and disturbances. The book intends to provide a unified platform for understanding and applicability of the fault-tolerant attitude control and control allocation for different purposes in aerospace engineering and some related fields. And it is particularly suited for readers who are interested to learn solutions in spacecraft attitude control system design and related engineering applications.
Presents the existing and emerging concepts concerning control allocation, and attitude control and fault-tolerant control for the over-actuated spacecraft under actuator failures Addresses the research problems Provides significant guidance to aerospace engineering Is simple, clear, and easy to read
Autor*in
Qinglei Hu
Themen in »Control Allocation for Spacecraft Under Actuator Faults«
Spacecraft Attitude Control Control Allocation Fault Tolerant Control Finite-Time Control Actuator Failures