Conference Program of WCICA 2012
Conference Program of WCICA 2012
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 𝛍 and<br />
𝛔 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 />
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