Transient Effects Related To Reconfigurable Control Design (Satellite Launcher)

Degraded performance and even instability may arise from faults or failures acting on a system. Sudden faults of small amplitude can also cause unacceptable results due to the transient amplification by controller gains, where linear working limits of system's components are exceeded. Fault Tol...

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Published inIFAC Proceedings Volumes Vol. 34; no. 15; pp. 79 - 84
Main Authors Ramos, F.O., Leite Filho, W.C.
Format Journal Article
LanguageEnglish
Published 01.09.2001
Subjects
fault tolerance
guidance systems
PI controllers
sensor failures
fault tolerance
guidance systems
PI controllers
sensor failures
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Abstract Degraded performance and even instability may arise from faults or failures acting on a system. Sudden faults of small amplitude can also cause unacceptable results due to the transient amplification by controller gains, where linear working limits of system's components are exceeded. Fault Tolerance requires not only the design of a suitable Fault Detection, Isolation and Reconfiguration (FDIR) scheme. It also demands for an intensive analysis regarding the effects of such faults or failures acting on the system, taking into account the new (reconfigured) control law. The current work illustrates this idea by considering the design of a Reconfigurable Controller for a satellite launcher subject to sensor faults.
AbstractList Degraded performance and even instability may arise from faults or failures acting on a system. Sudden faults of small amplitude can also cause unacceptable results due to the transient amplification by controller gains, where linear working limits of system's components are exceeded. Fault Tolerance requires not only the design of a suitable Fault Detection, Isolation and Reconfiguration (FDIR) scheme. It also demands for an intensive analysis regarding the effects of such faults or failures acting on the system, taking into account the new (reconfigured) control law. The current work illustrates this idea by considering the design of a Reconfigurable Controller for a satellite launcher subject to sensor faults.
Author Ramos, F.O.
Leite Filho, W.C.
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Cites_doi 10.1016/S0967-0661(97)00003-8
10.1016/0005-1098(76)90041-8
10.2514/3.21417
10.1016/S0967-0661(97)00053-1
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Keywords fault tolerance
guidance systems
PI controllers
sensor failures
Language English
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Snippet Degraded performance and even instability may arise from faults or failures acting on a system. Sudden faults of small amplitude can also cause unacceptable...
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SubjectTerms fault tolerance
guidance systems
PI controllers
sensor failures
Title Transient Effects Related To Reconfigurable Control Design (Satellite Launcher)
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