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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 />

Tang, Ying<br />

Yao, Wen-ji<br />

Wang, Zhang-quan<br />

Xu, Sen<br />

Zhejiang Shuren Univ.<br />

Zhejiang Shuren Univ.<br />

Zhejiang Shuren Univ.<br />

Zhejiang Shuren Univ.<br />

This work presents an open-loop, fully differential capacitive MEMS<br />

accelerometer implemented in CMOS technology. The mathematical<br />

model <strong>of</strong> this open-loop system is derived, which considers non-ideal<br />

factors in circuits such as nonlinear distortion and noises. These nonideal<br />

factors have been discussed through system level simulation using<br />

MATLAB. Simulation results show that the system has good capacitive<br />

sensitivity and is robust to noises. The detailed design <strong>of</strong> interface<br />

circuit in the proposed MEMS accelerometer is presented, using sigmadelta<br />

(Σ-Δ) modulation. Finally, the chip-level physical layout <strong>of</strong> interface<br />

circuit is implemented and tested, using silicon-on-insulator (SOI)<br />

substrate with 1μm CMOS process. Results have shown the chip with<br />

area <strong>of</strong> 1.32mm2 and power consumption <strong>of</strong> about 5mW. The proposed<br />

MEMS accelerometer is designed for acceleration <strong>of</strong> less than 5G, and<br />

its resolution is 1.923mG.<br />

◁ PSaC-92<br />

Attitude And Altitude Instrument Based On DSP, pp.5108–5111<br />

Xu, Peng<br />

Li, Baokui<br />

Geng, Qingbo<br />

Fei, Qing<br />

Beijing Inst. <strong>of</strong> Tech.<br />

Beijing Inst. <strong>of</strong> Tech.<br />

Beijing Inst. <strong>of</strong> Tech.<br />

Beijing Inst. <strong>of</strong> Tech.<br />

Unmanned Aerial Vehicle can be referred to as UAV .This design implements<br />

a system that based on DSP to measure altitude, airspeed and<br />

attitude <strong>of</strong> UAV. The system uses DSP as the controller and operator,<br />

and uses two MS5534C and a URF03-TTL232 to measure the altitude<br />

and airspeed <strong>of</strong> UAV. To measure attitude, we need three accelerometers<br />

and three gyroscopes. SCI serial port can be used to read data<br />

from the module. This design collects the data <strong>of</strong> these sensors by<br />

query method, and uses quaternion algorithm to calculate the attitude<br />

<strong>of</strong> UAV.<br />

◁ PSaC-93<br />

Study <strong>of</strong> Strong Tracking Augmented Unscented Kalman Filter in Integrated<br />

Navigation System., pp.5112–5115<br />

Xu, Dexin<br />

Wang, Lu<br />

Li, Guangchun<br />

Ma, Tao<br />

Harbin Engineering Univ.<br />

harbin engineering Univ.<br />

harbin engineering Univ.<br />

harbin engineering Univ.<br />

In order to solve the problem <strong>of</strong> inaccurate state estimation and divergent<br />

outputs <strong>of</strong> the filter <strong>of</strong> the low-cost integrated navigation system, a<br />

strong tracking augmented unscented kalman filter is proposed in this<br />

paper. This method extends the strong tracking filter principle into the<br />

augmented unscented kalman filter, which improves the strong tracking<br />

ability <strong>of</strong> the system states mutation. Using the state switching technology<br />

to reduce the dimension during the Sigma points’ sampling and<br />

this improves the real-time property <strong>of</strong> the filter. Applying this method<br />

into the low-cost integrated navigation system, the experiments results<br />

prove that this method can track the state mutation quickly and inhibit<br />

divergent outputs <strong>of</strong> the filter.<br />

◁ PSaC-94<br />

Research <strong>of</strong> Fault Diagnosis Based on Matching Pursuit and Biomimetic<br />

Pattern Recognition, pp.4848–4852<br />

Wang, Xiaozhe<br />

Wang, Jinping<br />

northeastern Univ.<br />

northeastern Univ.<br />

Abstract –Consider <strong>of</strong> influences <strong>of</strong> noise in sampling signals comprehensively,<br />

a method <strong>of</strong> fault diagnosis which combines matching pursuit<br />

(MP) and biomimetic pattern recognition (BPR) is put forward in<br />

this paper. Firstly, the matching pursuit (MP) algorithm is used to select<br />

optimum wavelets in different SNR situations from the Laplace wavelet<br />

dictionary. Then the feature vector is extracted according to the operation<br />

result <strong>of</strong> waveform MP and super high-dimensional detection<br />

feature spaces <strong>of</strong> biomimetic pattern recognition (BPR) is constructed.<br />

After that, the real-time detected partial discharge (PD) signals are<br />

cut, and the feature for each discharge pulse is extracted respectively,<br />

which realized the multiple fault recognition revolutionarily. Simulations<br />

show that the robustness and accuracy <strong>of</strong> fault pattern recognition is<br />

improved.<br />

204

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