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Conference Program of WCICA 2012

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<strong>Conference</strong> <strong>Program</strong> <strong>WCICA</strong> <strong>2012</strong><br />

Wang, Ping<br />

Liang, Fujun<br />

Qi, Shengbiao<br />

Tianjin Univ.<br />

Tianjin Univ.<br />

Tianjin Univ.<br />

When grid occurs short circuit fault and voltage drops, because <strong>of</strong> coupling<br />

relationships between stator and rotor windings <strong>of</strong> doubly-fed generator,<br />

over-current is generated in stator and rotor windings. At the<br />

same time, power that grid-side converter absorbs from the grid is out <strong>of</strong><br />

balance from the power that rotor-side converter outputs, which makes<br />

redundant energy accumulated in DC-link and leads to over-voltage<br />

and under-voltage produced. Over-current may damage rotor-side converter<br />

and makes wind turbine detach from grids, and DC-link capacitance<br />

will be break down for the over-voltage. Therefore, it is necessary<br />

to adopt protection circuit to realize the low voltage ride through <strong>of</strong> D-<br />

FIG system .In this paper, based on the established simulation model<br />

<strong>of</strong> DFIG, combination protection circuit composed <strong>of</strong> rotor-side Crowbar<br />

and DC-link protection circuit and it’s control strategy are researched<br />

during voltage drops for three symmetric short circuit fault <strong>of</strong> DFIG system,<br />

and simulated through Matlab/simulink s<strong>of</strong>tware.<br />

◁ PFrC-68<br />

Finite-Time Stabilization for a Class <strong>of</strong> Distributed Parameter Systems,<br />

pp.1948–1952<br />

FU, Qin<br />

Univ. <strong>of</strong> Sci. & Tech. <strong>of</strong> Suzhou<br />

The concept <strong>of</strong> finite-time stability and stabilization for distributed parameter<br />

systems is introduced by the definition <strong>of</strong> finite-time stability for<br />

linear systems.The design <strong>of</strong> state feedback controllers and dynamic<br />

output feedback controllers is given for a class <strong>of</strong> distributed parameter<br />

systems.A sufficient condition is provided by using linear matrix inequality(LMI).<br />

When the feedback control laws are applied to the systems,the<br />

closed-loop systems are finite-time stable.<br />

◁ PFrC-69<br />

On initial alignment <strong>of</strong> large azimuth misalignment for SINS on the static<br />

base in Krein space, pp.1964–1968<br />

FENG, JIN<br />

YU, FEI<br />

ZHANG, PENG-Yu<br />

Zou, Meikui<br />

Harbin Engineering Univ.<br />

Harbin Engineering Univ.<br />

Harbin Engineering Univ.<br />

Harbin Engineering Univ.<br />

The error equation for the azimuth misalignment angle for SINS on the<br />

static base is nonlinear, and it’s an urgent problem to align it when the<br />

angle is large. This paper proposes a method for the initial alignment<br />

<strong>of</strong> large azimuth misalignment based on Krein space linear estimation.<br />

The sum quadratic constraint (SQC) for nonlinear system is obtained<br />

by using Lipschitz condition <strong>of</strong> nonlinearity. Thus proposed Krein space<br />

approach is used to tackle the estimation problem for a class <strong>of</strong> nonlinear<br />

cases. Using kalman filter<strong>of</strong> krein space robust properties, we<br />

establish a nonlinear measurement error equation in Krein space, and<br />

give a recursive formula for the measurement error estimation. The<br />

initial alignment <strong>of</strong> large azimuth misalignment is simulated Finally, a<br />

numerical example is given to demonstrate the effectiveness <strong>of</strong> the<br />

proposed approach.By the Kalman filter method in Krein space which<br />

shows that the result generated by the Kalman frlter method in Krein<br />

space has effective and superior.<br />

◁ PFrC-70<br />

Research on QFT Controller Design for LOS Stabilization System <strong>of</strong><br />

Opto-electronic Load for UAV, pp.1982–1986<br />

Xu, Dexin<br />

Harbin Engineering Univ.<br />

HE, Kunpeng<br />

harbin engineering Univ.<br />

Wei, Yanhui<br />

harbin engineering Univ.<br />

Zhao, Jiangpeng Troops 92854<br />

In order to decrease affection <strong>of</strong> parameters uncertainty <strong>of</strong> line-<strong>of</strong>-sight<br />

stabilization system <strong>of</strong> opto-electronic load for UAV, quantitative feedback<br />

theory design method is adopted on the servo controller <strong>of</strong> line-<strong>of</strong>sight<br />

stabilization system <strong>of</strong> opto-electronic load for UAV. The simulation<br />

result indicates that the performance <strong>of</strong> QFT controller is better than<br />

the traditional controller. QFT method can deal with the special problem<br />

effectively since parameters uncertainty probably decrease control<br />

performance, it has strong robustness and can solve the controller design<br />

problem with parameters uncertainty <strong>of</strong> line-<strong>of</strong>-sight stabilization<br />

system <strong>of</strong> opto-electronic load for UAV.<br />

◁ PFrC-71<br />

Chaos Phenomenon in the DC-DC Switching Converters, pp.2039–<br />

2043<br />

Zhang, Yumei<br />

Qin, Hong<br />

Qu, Yanhua<br />

Wu, Jianhua<br />

Shenyang Inst. <strong>of</strong> Engineering<br />

Shenyang Inst. <strong>of</strong> Engineering<br />

Shenyang Inst. <strong>of</strong> Engineering<br />

Northeastern Univ.<br />

DC-DC switching converter is an important part <strong>of</strong> power electronics,<br />

belonging to strong nonlinear time-varying systems. In the course<br />

<strong>of</strong> their traditional research, which rarely involves the study <strong>of</strong> nonlinear<br />

phenomena. However, During switching converter is working state,<br />

it can produce a transient pulse containing high frequency harmonics<br />

that can emit electromagnetic interference, electromagnetic interference<br />

can cause pollution to the network and direct impact to other electrical<br />

appliances to work by conduction, radiation, all these phenomena<br />

indicates that the existence <strong>of</strong> chaos. Because chaos is a state as a<br />

result <strong>of</strong> instability, the uncertainty will lead the operation <strong>of</strong> the system<br />

to phenomena like Random, which affect the control performance <strong>of</strong><br />

converter, even lead to not working, the study <strong>of</strong> chaos in the switching<br />

converter and its control methods which have important guiding significance<br />

in the correct designing and debugging switching converter will<br />

help us to avoid or eliminate this phenomenon in the design, so that the<br />

converter works in a stable cycle.<br />

◁ PFrC-72<br />

Adaptive Integral-Type Sliding Mode Control for a Class <strong>of</strong> Uncertain<br />

Nonlinear Systems, pp.2081–2084<br />

Sun, Li-Ying<br />

Liaoning Univ. <strong>of</strong> Tech.<br />

An integral-type sliding mode control method for a class <strong>of</strong> uncertain<br />

nonlinear systems in parameter feedback form is developed. The design<br />

procedure can be divided into two steps. Firstly, design a nonlinear<br />

integral-type sliding manifold for the uncertain system such that not only<br />

the sliding motion can occur on that manifold, but also the system’<br />

s motion along the manifold is asymptotically stable. The integral-type<br />

sliding surface is constructed by adding an integral term into the linear<br />

sliding surface. The additional integral in the proposed sliding surface<br />

provides one more degree <strong>of</strong> freedom; Secondly, based on the Lyapunov<br />

stability theorem, design a control law, such that the system’s<br />

states are driven towards the manifold and stay there for all future time,<br />

regardless <strong>of</strong> uncertainties.<br />

◁ PFrC-73<br />

Exponential Synchronization <strong>of</strong> a Class <strong>of</strong> Chaotic Neural Network,<br />

pp.2194–2197<br />

Qiao, Zongmin<br />

Zhang, Pei<br />

Hefei Normal Univ.<br />

anhui Univ.<br />

Synchronization <strong>of</strong> chaotic system has become an important area <strong>of</strong><br />

study. A chaotic system is a nonlinear deterministic system that possesses<br />

complex and unpredictable behaviour. Based on nonlinear state<br />

coupling, this paper derived a delay independent sufficient exponential<br />

synchronization condition based on the Lyapunov stability method and<br />

the Halanay inequality lemma. The proposed condition is less conservative<br />

than previously established ones in the literature.<br />

◁ PFrC-74<br />

Adaptive Observer Design for a Class <strong>of</strong> MIMO Nonlinear Systems,<br />

pp.2198–2203<br />

ZHAO, Lili<br />

Li, Ping<br />

LI, Xiuliang<br />

Zhejiang Univ.<br />

Zhejiang Univ.<br />

Zhejiang Univ.<br />

For a class <strong>of</strong> uniformly observable nonlinear multi-input-multi-output<br />

(MIMO) systems with unknown parameters in both state and output e-<br />

quations, an adaptive observer is designed in a constructive manner<br />

based on the techniques <strong>of</strong> high gain observer and adaptive estimation.<br />

The high gain adaptive observer for joint state and unknown pa-<br />

144

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