Method of Successive Approximations for Optimal Control under Uncertainty of Initial Data: An Interval Approach

This article discusses the development of an interval algorithm based on the method of successive approximations for solving optimal control problems under uncertainty of initial data. To achieve this goal, interval analysis methods are applied, allowing for the consideration of variations in system parameters. A numerical implementation of the algorithm is provided, along with a description of a computational experiment using a model example. The results demonstrate that the proposed method can construct confidence intervals for the solutions to the optimal control problem, making it useful for practical applications in situations with uncertainty in initial parameters.

Authors

Publication Details

Published
2024-11-13
DOI
https://doi.org/10.1109/summa64428.2024.10803887
Primary Topic
Aerospace Engineering and Control Systems
Type
article
Field-Weighted Citation Impact
0.00

Funders

Controls
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article

Method of Successive Approximations for Optimal Control under Uncertainty of Initial Data: An Interval Approach

Э. Р. Гиззатова, Tatiana Mikhaylova, Sofia Mustafina
Aerospace Engineering and Control Systems
article

Method of Successive Approximations for Optimal Control under Uncertainty of Initial Data: An Interval Approach

Э. Р. Гиззатова, Tatiana Mikhaylova, Sofia Mustafina
article en

Abstract

This article discusses the development of an interval algorithm based on the method of successive approximations for solving optimal control problems under uncertainty of initial data. To achieve this goal, interval analysis methods are applied, allowing for the consideration of variations in system parameters. A numerical implementation of the algorithm is provided, along with a description of a computational experiment using a model example. The results demonstrate that the proposed method can construct confidence intervals for the solutions to the optimal control problem, making it useful for practical applications in situations with uncertainty in initial parameters.

Russian Science Foundation
Openalex Percentile: Top 59%
Aerospace Engineering and Control Systems
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