Institute of Electrical and Electronics Engineers (IEEE)

27195

Автор(ы): 

Автор(ов): 

2

Параметры публикации

Тип публикации: 

Доклад

Название: 

A Novel Approach for Scheduling in STDMA for High-Throughput Backbone Wireless Mesh Networks Operating within 60-80 GHz

ISBN/ISSN: 

ISBN 978-1-4244-7508-7

Наименование конференции: 

  • 3th International Conference on Advances in Mesh Networks (MESH'2010, Venice)

Наименование источника: 

  • Proceedings of the 3th International Conference «Advances in Mesh Networks» (MESH'2010, Venice)

Город: 

  • Венеция

Издательство: 

  • Institute of Electrical and Electronics Engineers (IEEE)

Год издания: 

2010

Страницы: 

86-91
Аннотация
This work proposes a novel approach to centralized scheduling in Spatial TDMA (STDMA) for a new class of high-throughput backbone broadband wireless mesh networks operating within 60-80 GHz. The approach is based on granted-to-requested ratio maxmin optimization criterion. During a research work, a centralized gradient algorithm for an optimal schedule construction was developed and its polynomial convergence was proven. The paper outlines key features of the highthroughput wireless mesh networks class under development, contains the scheduling problem formulation and introduces the polynomial algorithm for optimal resource allocation.

Библиографическая ссылка: 

Вишневский В.М., Ларионов А.А. A Novel Approach for Scheduling in STDMA for High-Throughput Backbone Wireless Mesh Networks Operating within 60-80 GHz / Proceedings of the 3th International Conference «Advances in Mesh Networks» (MESH'2010, Venice). Венеция: Institute of Electrical and Electronics Engineers (IEEE), 2010. С. 86-91.

17611

Автор(ы): 

Автор(ов): 

2

Параметры публикации

Тип публикации: 

Доклад

Название: 

Minimization of the unmatched disturbances in the sliding mode control systems via invariant ellipsoid method

ISBN/ISSN: 

1085-1992

Наименование конференции: 

  • 3rd IEEE Multi-conference on Systems and Control (MSC 2009, Saint-Petersburg)

Наименование источника: 

  • Proceedings of IEEE 3th Multi Conference on Systems and Control (MSC 2009, Saint-Petersburg)

Город: 

  • Санкт-Петербург

Издательство: 

  • Institute of Electrical and Electronics Engineers (IEEE)

Год издания: 

2009

Страницы: 

1122-1127, http://ieeexplore.ieee.org/xpl/articleDetails.jsp?arnumber=5280842
Аннотация
The new sliding mode control design algorithm for a linear disturbed system is presented. It is based on the appropriate selection of the sliding surface via invariant ellipsoid method. The designed control guarantees minimization of the effects of unmatched disturbances to the system motion in the sliding mode. All theoretical results are approved by numerical simulations.

Библиографическая ссылка: 

Поляков А.Е., Позняк А.С. Minimization of the unmatched disturbances in the sliding mode control systems via invariant ellipsoid method / Proceedings of IEEE 3th Multi Conference on Systems and Control (MSC 2009, Saint-Petersburg). СПб.: Institute of Electrical and Electronics Engineers (IEEE), 2009. С. 1122-1127, http://ieeexplore.ieee.org/xpl/articleDetails.jsp?arnumber=5280842.

17610

Автор(ы): 

Автор(ов): 

3

Параметры публикации

Тип публикации: 

Доклад

Название: 

Output Linear Controller for a Class of Nonlinear Systems Using the Invariant Ellipsoid Method

ISBN/ISSN: 

0743-1619

Наименование конференции: 

  • 2009 American Control Conference (ACC2009, St. Louis)

Наименование источника: 

  • Proceedings of American Control Conference (IEEE ACC-2009, St. Louis)

Город: 

  • Сент-Луис, США

Издательство: 

  • Institute of Electrical and Electronics Engineers (IEEE)

Год издания: 

2009

Страницы: 

1160-1165, http://ieeexplore.ieee.org/xpl/articleDetails.jsp?arnumber=5160434
Аннотация
This paper deals with the problem of robust stabilization of an uncertain nonlinear system with output measurements using the invariant ellipsoid method. The non-linear system is uncertain but bounded according to a dasiaquasi-lipschitzpsila condition and the output measurements are subjected to perturbations bounded by ellipsoids.The invariant ellipsoid method allows to obtain the robust linear feedback as a solution of the special linear optimization problem with bilinear constraints. The methods for solving this optimization problem involves the LMI technique. The stabilization of the double mass-spring system is considered as an illustrative example.

Библиографическая ссылка: 

Гонсалес-Гарсия С., Поляков А.Е., Позняк А.С. Output Linear Controller for a Class of Nonlinear Systems Using the Invariant Ellipsoid Method / Proceedings of American Control Conference (IEEE ACC-2009, St. Louis). Сент-Луис, США: Institute of Electrical and Electronics Engineers (IEEE), 2009. С. 1160-1165, http://ieeexplore.ieee.org/xpl/articleDetails.jsp?arnumber=5160434.

17608

Автор(ы): 

Автор(ов): 

3

Параметры публикации

Тип публикации: 

Доклад

Название: 

Linear feedback spacecraft stabilization using the method of invariant ellipsoids

ISBN/ISSN: 

0094-2898

Наименование конференции: 

  • 41st Southeastern Symposium on System Theory (IEEE SSST-2009, Tullahoma, Tennessee, USA)

Наименование источника: 

  • Proceedings of the 41st Southeastern Symposium on System Theory (IEEE SSST-2009, Tullahoma, Tennessee, USA)

Город: 

  • Туллахома, США

Издательство: 

  • Institute of Electrical and Electronics Engineers (IEEE)

Год издания: 

2009

Страницы: 

195-198, http://ieeexplore.ieee.org/xpl/articleDetails.jsp?arnumber=4806834
Аннотация
This paper addresses the robust attitude control for an uncertain flexible spacecraft with disturbances bounded by ellipsoids. An observed-state feedback is designed using the so-called invariant ellipsoid method, which is based on the local invariant set theorem. The minimum invariant ellipsoid can be considered as the influence of the uncertainties and disturbances in the controlled system. All these considerations were expressed through LMI technique as an optimization problem with linear objective and LMI constraints. The numerical solution of this problem gives the parameters for the linear controller and the Luenberger observer that guarantee a quasi-minimal invariant ellipsoid for the controlled spacecraft.

Библиографическая ссылка: 

Гонсалес-Гарсия С., Поляков А.Е., Позняк А.С. Linear feedback spacecraft stabilization using the method of invariant ellipsoids / Proceedings of the 41st Southeastern Symposium on System Theory (IEEE SSST-2009, Tullahoma, Tennessee, USA). Туллахома, США: Institute of Electrical and Electronics Engineers (IEEE), 2009. С. 195-198, http://ieeexplore.ieee.org/xpl/articleDetails.jsp?arnumber=4806834.

17606

Автор(ы): 

Автор(ов): 

2

Параметры публикации

Тип публикации: 

Статья в журнале/сборнике

Название: 

Reaching Time Estimation for "Super-Twisting" Second Order Sliding Mode Controller via Lyapunov Function Designing

ISBN/ISSN: 

0018-9286

Наименование источника: 

  • IEEE Transactions on Automatic Control

Обозначение и номер тома: 

Т. 54, № 8

Город: 

  • Нью-Йорк

Издательство: 

  • Institute of Electrical and Electronics Engineers (IEEE)

Год издания: 

2009

Страницы: 

1951-1955
Аннотация
A method of a Lyapunov functions design based on resolving of the first-order partial differential equation of a special type is presented. A successful resolution of this equation guaranties a finite-time convergence for the corresponding dynamics given by an ordinary differential equation with a discontinuous right-hand side. It is also provides an analytical formula for an upper bound of the corresponding reaching time. The suggested method is applied to the problem of a stability analysis and a reaching time estimation of the, so-called, "super-twisting" controller. The estimation accuracy is confirmed by numerical example.

Библиографическая ссылка: 

Поляков А.Е., Позняк А.С. Reaching Time Estimation for "Super-Twisting" Second Order Sliding Mode Controller via Lyapunov Function Designing // IEEE Transactions on Automatic Control. 2009. Т. 54, № 8. С. 1951-1955.

17584

Автор(ы): 

Автор(ов): 

2

Параметры публикации

Тип публикации: 

Доклад

Название: 

The Mirror Descent Control Algorithm for Weakly Regular Homogeneous Finite Markov Chains with Unknown Mean Losses

Электронная публикация: 

Да

ISBN/ISSN: 

0743-1546

Наименование конференции: 

  • 50th IEEE Conference on Decision and Control and European Control Conference (CDC-ECC-2011, Orlando, Fl)

Наименование источника: 

  • Proceedings of the 50th IEEE Conference on Decision and Control and European Control Conference (CDC-ECC-2011, Orlando, Fl)

Город: 

  • Орландо, США

Издательство: 

  • Institute of Electrical and Electronics Engineers (IEEE)

Год издания: 

2011

Страницы: 

1779-1783
Аннотация
We address the adaptive stochastic control problem for a discrete time system described by controlled Markov chain with finite number of states. The mirror descent randomized control algorithm on the class of controlled homogeneous finite Markov chains with unknown mean losses has been proposed and studied. Here we develop the approach represented in Nazin and Miller (2011). The main assumptions are the following: processes are independent and stationary, nonnegative random losses are almost surely bounded by a given constant, and the connectivity assumption for the controlled Markov chain holds. The uncertainty is that the mean loss matrix is unknown. The novelty of the approach is in extension of the class of controlled homogeneous finite Markov chains to the chains with connectivity assumption. The main result consists in demonstration of the asymptotical upper bound as the time tends to infinity and in determining of the explicit constant which is weakly depending on the logarithm of the number of states.

Библиографическая ссылка: 

Назин А.В., Миллер Б.М. The Mirror Descent Control Algorithm for Weakly Regular Homogeneous Finite Markov Chains with Unknown Mean Losses / Proceedings of the 50th IEEE Conference on Decision and Control and European Control Conference (CDC-ECC-2011, Orlando, Fl). Орландо, США: Institute of Electrical and Electronics Engineers (IEEE), 2011. С. 1779-1783.

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