ON SINGULARITIES OF A-ORBITAL FEEDBACK LINEARIZATION OF SINGLE-INPUT AFFINE CONTROL SYSTEMS

For single-input affine control systems, we address the problem of A-orbital feedback linearization around singular points of the derived flag of the distribution associated with the control system. By a singular point of a derived flag we mean a point such that at least one of the elements of the derived flag in any neighborhood of this point is not a distribution of constant rank. We prove a local necessary and sufficient condition for A-orbital feedback equivalence of a single-input affine control system to a linear controllable system considered in a neighbourhood of the zero equilibrium point.

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Publication Details

Journal
Дифференциальные уравнения / Differential Equations
Published
2025-01-01
DOI
https://doi.org/10.7868/s3034503025030078
Primary Topic
Aerospace Engineering and Control Systems
Type
article
Field-Weighted Citation Impact
0.00
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article

ON SINGULARITIES OF A-ORBITAL FEEDBACK LINEARIZATION OF SINGLE-INPUT AFFINE CONTROL SYSTEMS

Д. А. Фетисов
Дифференциальные уравнения / Differential Equations
Aerospace Engineering and Control Systems
article

ON SINGULARITIES OF A-ORBITAL FEEDBACK LINEARIZATION OF SINGLE-INPUT AFFINE CONTROL SYSTEMS

Д. А. Фетисов
article en

Abstract

For single-input affine control systems, we address the problem of A-orbital feedback linearization around singular points of the derived flag of the distribution associated with the control system. By a singular point of a derived flag we mean a point such that at least one of the elements of the derived flag in any neighborhood of this point is not a distribution of constant rank. We prove a local necessary and sufficient condition for A-orbital feedback equivalence of a single-input affine control system to a linear controllable system considered in a neighbourhood of the zero equilibrium point.

Дифференциальные уравнения / Differential EquationsVol. 61(3)
Openalex Percentile: Top 65%
Aerospace Engineering and Control Systems
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