Решение граничной задачи для нелинейной стационарной управляемой системы на бесконечном промежутке времени с учетом дискретности управления

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Решение граничной задачи для нелинейной стационарной управляемой системы на бесконечном промежутке времени с учетом дискретности управления. / Квитко, А.Н.; Якушева, Д.Б.

In: ИНФОРМАЦИОННО-УПРАВЛЯЮЩИЕ СИСТЕМЫ, No. 6, 2011, p. 25-29.

Research output: Contribution to journal › Article

BibTeX

@article{80f06424f06b4bbea9fbf1fd7ca79c73,

title = "Решение граничной задачи для нелинейной стационарной управляемой системы на бесконечном промежутке времени с учетом дискретности управления",

abstract = "By constructing an asymptotic observer of Luenberger type, we develop a method for finding the control function that guarantees to transfer a wide class of nonlinear nonstationary controllable systems of ordinary differential equations from the initial state to a given final state according to the actually measured values, constraints on the control, and nonlinearities in the sensor equation. We find a constructive criterion that guarantees the existence of a solution for this problem. We also consider the problem of interorbital space flight.",

author = "А.Н. Квитко and Д.Б. Якушева",

year = "2011",

language = "не определен",

pages = "25--29",

journal = "ИНФОРМАЦИОННО-УПРАВЛЯЮЩИЕ СИСТЕМЫ",

issn = "1684-8853",

publisher = "Санкт-Петербургский государственный университет аэрокосмического приборостроения",

number = "6",

}

RIS

TY - JOUR

T1 - Решение граничной задачи для нелинейной стационарной управляемой системы на бесконечном промежутке времени с учетом дискретности управления

AU - Квитко, А.Н.

AU - Якушева, Д.Б.

PY - 2011

Y1 - 2011

N2 - By constructing an asymptotic observer of Luenberger type, we develop a method for finding the control function that guarantees to transfer a wide class of nonlinear nonstationary controllable systems of ordinary differential equations from the initial state to a given final state according to the actually measured values, constraints on the control, and nonlinearities in the sensor equation. We find a constructive criterion that guarantees the existence of a solution for this problem. We also consider the problem of interorbital space flight.

AB - By constructing an asymptotic observer of Luenberger type, we develop a method for finding the control function that guarantees to transfer a wide class of nonlinear nonstationary controllable systems of ordinary differential equations from the initial state to a given final state according to the actually measured values, constraints on the control, and nonlinearities in the sensor equation. We find a constructive criterion that guarantees the existence of a solution for this problem. We also consider the problem of interorbital space flight.

M3 - статья

SP - 25

EP - 29

JO - ИНФОРМАЦИОННО-УПРАВЛЯЮЩИЕ СИСТЕМЫ

JF - ИНФОРМАЦИОННО-УПРАВЛЯЮЩИЕ СИСТЕМЫ

SN - 1684-8853

IS - 6

ER -

ID: 5498083