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Solving Boundary Value Problem for a Nonlinear Stationary Controllable System with Synthesizing Control. / Kvitko, Alexander N.; Firyulina, Oksana S.; Eremin, Alexey S.

In: Mathematical Problems in Engineering, Vol. 2017, 8529760, 2017.

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@article{aeb7cf6fa0d84eedb72009e8b87f9487,
title = "Solving Boundary Value Problem for a Nonlinear Stationary Controllable System with Synthesizing Control",
abstract = "An algorithm for constructing a control function that transfers a wide class of stationary nonlinear systems of ordinary differential equations from an initial state to a final state under certain control restrictions is proposed. The algorithm is designed to be convenient for numerical implementation. A constructive criterion of the desired transfer possibility is presented. The problem of an interorbital flight is considered as a test example and it is simulated numerically with the presented method.",
author = "Kvitko, {Alexander N.} and Firyulina, {Oksana S.} and Eremin, {Alexey S.}",
year = "2017",
doi = "10.1155/2017/8529760",
language = "English",
volume = "2017",
journal = "Mathematical Problems in Engineering",
issn = "1024-123X",
publisher = "Hindawi ",

}

RIS

TY - JOUR

T1 - Solving Boundary Value Problem for a Nonlinear Stationary Controllable System with Synthesizing Control

AU - Kvitko, Alexander N.

AU - Firyulina, Oksana S.

AU - Eremin, Alexey S.

PY - 2017

Y1 - 2017

N2 - An algorithm for constructing a control function that transfers a wide class of stationary nonlinear systems of ordinary differential equations from an initial state to a final state under certain control restrictions is proposed. The algorithm is designed to be convenient for numerical implementation. A constructive criterion of the desired transfer possibility is presented. The problem of an interorbital flight is considered as a test example and it is simulated numerically with the presented method.

AB - An algorithm for constructing a control function that transfers a wide class of stationary nonlinear systems of ordinary differential equations from an initial state to a final state under certain control restrictions is proposed. The algorithm is designed to be convenient for numerical implementation. A constructive criterion of the desired transfer possibility is presented. The problem of an interorbital flight is considered as a test example and it is simulated numerically with the presented method.

UR - http://www.scopus.com/inward/record.url?scp=85030753659&partnerID=8YFLogxK

U2 - 10.1155/2017/8529760

DO - 10.1155/2017/8529760

M3 - Article

AN - SCOPUS:85030753659

VL - 2017

JO - Mathematical Problems in Engineering

JF - Mathematical Problems in Engineering

SN - 1024-123X

M1 - 8529760

ER -

ID: 14857642