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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 />

A comparison study on TDOA based localization algorithms for sensor<br />

networks, pp.4490–4495<br />

Qu, Xiaomei<br />

Xie, Lihua<br />

Nanyang Technological Univ.<br />

Nanyang Technological Univ.<br />

For the purpose <strong>of</strong> source localization, we have proposed two recursive<br />

algorithms in our companion paper, which use time difference <strong>of</strong> arrival<br />

(TDOA) measurements received from sensors by accounting for random<br />

uncertainties in sensor positions. This paper is devoted to presenting<br />

a comparative analysis on the two recursive localization algorithms.<br />

The first algorithm is called recursive localization algorithm, which uses<br />

the current estimate <strong>of</strong> source position to form a new measurement<br />

equation <strong>of</strong> the unknown source position. The second algorithm firstly<br />

estimates an auxiliary variable and then rearranges the nonlinear T-<br />

DOA equation into a linear measurement equation. By employing the<br />

update covariance <strong>of</strong> the update localization <strong>of</strong> the two algorithms, it is<br />

shown that the second algorithm outperforms the first one. An illustrative<br />

example is included to validate our theoretic results.<br />

◮ SuB10-2 16:10–16:30<br />

Robust Stabilization <strong>of</strong> Networked Control Systems with Multiple-packet<br />

Transmission via Jump System Approach, pp.4496–4501<br />

Ding, Nan<br />

Yu, Mei<br />

Yuan, Xiaodan<br />

Li, Jie<br />

Yu, Junyan<br />

North China Electric Power Univ.<br />

North China Electric Power Univ.<br />

North China Electric Power Univ.<br />

North China Electric Power Univ.<br />

Univ. <strong>of</strong> Electronic Sci. ang Tech. in China<br />

A jump system approach to stabilization and robust stabilization <strong>of</strong> networked<br />

control systems (NCSs) with multiple-packet transmissions are<br />

addressed. We focus our attention on the case that the packets are<br />

transmitted via limited capacity communication channels. Sufficient<br />

conditions on the mean square stabilization <strong>of</strong> NCSs are obtained in<br />

terms <strong>of</strong> linear matrix inequalities (LMIs). Non-fragile state feedback<br />

controller can be constructed directly via LMIs. A numerical example is<br />

worked out to demonstrate the effectiveness <strong>of</strong> the proposed method.<br />

◮ SuB10-3 16:30–16:50<br />

Distributed fusion filter for multi-rate multi-sensor systems with packet<br />

dropouts, pp.4502–4506<br />

Ma, Jing<br />

Sun, Shuli<br />

Heilongjiang Univ.<br />

Heilongjiang Univ.<br />

This paper is concerned with the distributed fusion filtering problem for<br />

a class <strong>of</strong> asynchronous multi-rate multi-sensor systems with different<br />

packet dropout rates, where the system is described at the highest<br />

sampling rate and different sensors may have different measurement<br />

sampling rates. Firstly, the multi-rate fusion estimation problem is<br />

transformed into an equivalent single rate fusion estimation problem<br />

using a “dummy”measurement. Then, the optimal distributed fusion<br />

filter is given based on the well-known optimal fusion algorithm weighted<br />

by matrices in the linear minimum variance sense. The filtering error<br />

cross-covariance matrix is derived between any two subsystems. Simulation<br />

research verifies the effectiveness <strong>of</strong> the proposed filter.<br />

◮ SuB10-4 16:50–17:10<br />

Self-learning sensor scheduling for target tracking in wireless sensor<br />

networks based on adaptive dynamic programming, pp.1056–1061<br />

Xiao, Wendong<br />

Song, Ruizhuo<br />

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

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

This paper proposes a novel self-learning sensor scheduling scheme,<br />

which makes the sensor energy consumption and sensor tracking error<br />

optimal over the system operational horizon. The scheme employs<br />

Kalman filter estimation technique to predict the tracking accuracy. A<br />

performance index function is established based on the predicted energy<br />

consumption and tracking error. A self-learning scheduling method<br />

is proposed based on adaptive dynamic programming algorithm. The<br />

numerical example shows the effectiveness <strong>of</strong> the proposed approach.<br />

◮ SuB10-5 17:10–17:30<br />

A New Approach to Quantized Stabilization <strong>of</strong> Stochastic System with<br />

Multiplicative Noise, pp.2382–2387<br />

Wei, Li<br />

Zhang, Huanshui<br />

Shandong Univ.<br />

Shandong Univ.<br />

A new quantization dependent Lyapunov function is proposed to analysis<br />

the quantized feedback stabilization problem <strong>of</strong> discrete-time system<br />

with multiplicative noises. For convenience <strong>of</strong> the pro<strong>of</strong>, only singleinput<br />

case is considered (which can be generalized to multi-input channel),<br />

conditions for the system to be mean-square poly-quadratic stabilized<br />

are derived as well as the analysis <strong>of</strong> H-inf performance and controller<br />

design for the given stochastic system with logarithmic quantizer.<br />

The most significant feature is the utilization <strong>of</strong> a quantization dependent<br />

Lyapunov function, leading to less conservative results, which is<br />

shown both theoretically and through numerical examples.<br />

◮ SuB10-6 17:30–17:50<br />

Outlier Detection in Heart Rate Signal using Activity information,<br />

pp.4511–4516<br />

Yang, Yuanjing<br />

Ji, Lianying<br />

Wu, Jian Kang<br />

Graduated Univ. <strong>of</strong> Chinese Acad. <strong>of</strong> Sci.<br />

Graduate Univ. <strong>of</strong> Chinese Acad. <strong>of</strong> Sci.<br />

Graduate Univ., Chinese Acad. <strong>of</strong> Sci.<br />

During exercise, heart rate will increase and its distribution will be different<br />

from that in stationary statement. Moreover, activity introduces<br />

several outliers into heart rate series. Heart rate variability analysis<br />

under exercise conditions can’t be conducted identically to the traditional<br />

methods. A heart rate distribution analysis method is proposed<br />

to fuse the activity information and heart rate signals which will be used<br />

to make heart rate analysis under exercise conditions. Firstly we use<br />

Gaussian function to fit RR intervals under various intensity activities,<br />

and then establish dynamic model for the parameter &#120525; and<br />

&#120532; which is changed with activity intensity. With the distribution<br />

<strong>of</strong> heart rate determined, outliers in RR interval can be detected<br />

and replaced according to possibility distribution. In the last, the validity<br />

<strong>of</strong> outlier detection algorithm and the influence <strong>of</strong> outliers to HRV are<br />

verified.<br />

SuB11 16:10–17:50 Room 311C<br />

Invited Session: Hypersonic flight control<br />

Chair: Chen, Mou<br />

Co-Chair: Duan, Haibin<br />

NUAA<br />

Beihang Univ.<br />

◮ SuB11-1 16:10–16:30<br />

Modeling and Control for Near-Space Vehicles With Oblique Wing,<br />

pp.1773–1778<br />

Pang, Jie<br />

Rong, Mei<br />

Chen, Mou<br />

NUAA<br />

Nanjing Univ. <strong>of</strong> Aeronautics & Astronautics<br />

NUAA<br />

In this paper, the flight motion model for near-space vehicle with an<br />

oblique wing is presented, and the flight control system is developed<br />

using dynamic inversion method. Firstly, based on its asymmetry<br />

configuration and special aerodynamic characteristic, the six-degree<strong>of</strong>-freedom<br />

nonlinear equations <strong>of</strong> flight motion are derived using Newton’s<br />

second law and law <strong>of</strong> inertia via considering the influence <strong>of</strong><br />

oblique wing. Secondly, the dynamic inversion control scheme is designed<br />

for the near-space vehicle with an oblique wing. Finally, simulation<br />

results are presented to illustrate the effectiveness <strong>of</strong> the proposed<br />

flight control scheme.<br />

◮ SuB11-2 16:30–16:50<br />

Attitude Quaternion Control in the Final Approach Phase <strong>of</strong> Rendezvous<br />

and Docking by Sliding Mode Control, pp.2177–2181<br />

Zong, Xiaoxiao<br />

Liu, Zhenghua<br />

Ren, Yan<br />

Li, Nan<br />

Beihang Univ.<br />

School <strong>of</strong> Automation<br />

Beihang Univ.<br />

Beihang Univ.<br />

For the relative attitude control problem in phasing period <strong>of</strong> rendezvous<br />

and docking, attitude quaternion was adopted to describe the dynamic<br />

model and the kinematics equation <strong>of</strong> spacecraft. Then attitude quaternion<br />

PD feedback was designed to control the relative attitude successfully.<br />

On this basis, the sliding mode control was researched and<br />

used in relative attitude control to improve accuracy and build up anti-<br />

222

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