Robust orbital stabilization: A Floquet theory–based approach

The design of robust orbitally stabilizing feedback is considered. From a known orbitally stabilizing controller for a nominal, disturbance‐free system, a robustifying feedback extension is designed utilizing the sliding‐mode control (SMC) methodology. The main contribution of the article is to prov...

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Published inInternational journal of robust and nonlinear control Vol. 31; no. 16; pp. 8075 - 8108
Main Authors Sætre, Christian Fredrik, Shiriaev, Anton S., Freidovich, Leonid B., Gusev, Sergei V., Fridman, Leonid M.
Format Journal Article
LanguageEnglish
Published Bognor Regis Wiley Subscription Services, Inc 10.11.2021
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Online AccessGet full text
ISSN1049-8923
1099-1239
1099-1239
DOI10.1002/rnc.5738

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Abstract The design of robust orbitally stabilizing feedback is considered. From a known orbitally stabilizing controller for a nominal, disturbance‐free system, a robustifying feedback extension is designed utilizing the sliding‐mode control (SMC) methodology. The main contribution of the article is to provide a constructive procedure for designing the time‐invariant switching function used in the SMC synthesis. More specifically, its zero‐level set (the sliding manifold) is designed using a real Floquet–Lyapunov transformation to locally correspond to an invariant subspace of the Monodromy matrix of a transverse linearization. This ensures asymptotic stability of the periodic orbit when the system is confined to the sliding manifold, despite any system uncertainties and external disturbances satisfying a matching condition. The challenging task of oscillation control of the underactuated cart–pendulum system subject to both matched‐ and unmatched disturbances/uncertainties demonstrates the efficacy of the proposed scheme.
AbstractList The design of robust orbitally stabilizing feedback is considered. From a known orbitally stabilizing controller for a nominal, disturbance‐free system, a robustifying feedback extension is designed utilizing the sliding‐mode control (SMC) methodology. The main contribution of the article is to provide a constructive procedure for designing the time‐invariant switching function used in the SMC synthesis. More specifically, its zero‐level set (the sliding manifold) is designed using a real Floquet–Lyapunov transformation to locally correspond to an invariant subspace of the Monodromy matrix of a transverse linearization. This ensures asymptotic stability of the periodic orbit when the system is confined to the sliding manifold, despite any system uncertainties and external disturbances satisfying a matching condition. The challenging task of oscillation control of the underactuated cart–pendulum system subject to both matched‐ and unmatched disturbances/uncertainties demonstrates the efficacy of the proposed scheme.
Author Fridman, Leonid M.
Freidovich, Leonid B.
Sætre, Christian Fredrik
Shiriaev, Anton S.
Gusev, Sergei V.
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Snippet The design of robust orbitally stabilizing feedback is considered. From a known orbitally stabilizing controller for a nominal, disturbance‐free system, a...
The design of robust orbitally stabilizing feedback is considered. From a known orbitally stabilizing controller for a nominal, disturbance-free system, a...
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SubjectTerms Disturbances
Feedback
Invariants
Manifolds
Orbital stability
orbital stabilization
Orbits
robust nonlinear control
Robustness
Sliding
sliding mode control
Uncertainty
underactuated mechanical systems
Title Robust orbital stabilization: A Floquet theory–based approach
URI https://onlinelibrary.wiley.com/doi/abs/10.1002%2Frnc.5738
https://www.proquest.com/docview/2582033294
https://urn.kb.se/resolve?urn=urn:nbn:se:umu:diva-187289
Volume 31
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