• 한국정보통신학회논문지
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• 제13권5호
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• pp.854-859
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• 2009

USN(Ubiquitous Sensor Network)을 이용한 많은 시범사업들이 진행되었으며, 최근에는 환경감시 분야에서 활용이 많은 관심을 받고 있다. USN의 센서노드로부터 정보를 획득하기 위해서는 RF 송수신기가 반드시 필요하다. 본 논문은 IEEE 802.15.4의 규격을 만족하면서 2.4GHz 대역에서 동작하는 센서노드용 RF 송수신기의 설계에 대해서 기술한다. 본 논문에는 구현하려는 송수신기의 구조와 IEEE 802.15.4의 요구 규격이 기술되어 있으며, 이 규격으로부터 도출된 RF 송수신기의 설계 파라미터로써 수신기의 잡음지수, 필터의 선택도, 주파수합성기의 위상잡음, 송신기의 선형성과 스펙트럼 마스크가 기술되어 있다.

• Current Optics and Photonics
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• 제2권4호
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• pp.303-307
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• 2018

We propose a simple ultraviolet (UV) sensor consisting of a conventional single-mode optical fiber capped with an azobenzene-moiety-containing polymer. The UV light changes the dimensions of the azobenzene polymer, as well as the refractive index of the material. Incident light with a wavelength of 1550 nm was reflected at the fiber/polymer and polymer/air interfaces, and interference of the reflected beams resulted in spectral interference that shifted the wavelength by 0.78 nm at a UV input power of $2.5mW/cm^2$. The UV sensor's response to wavelength is nonlinear and stable. The response speed of the sensor is limited by detection noise, which can be improved by modifying the insertion loss of the UV sensor and the signal-to-noise ratio of the detection system. The proposed compact UV sensor is easy to fabricate, is not susceptible to electromagnetic interference, and only reacts to UV light.

• International Journal of Aeronautical and Space Sciences
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• 제8권1호
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• pp.10-20
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• 2007

For spacecraft attitude control, reaction wheel (RW) steering laws with more than three wheels for three-axis attitude control can be derived by using a control allocation (CA) approach.1-2 The CA technique deals with a problem of distributing a given control demand to available sets of actuators.3-4 There are many references for CA with applications to aerospace systems. For spacecraft, the control torque command for three body-fixed reference frames can be constructed by a combination of multiple wheels, usually four-wheel pyramid sets. Multi-wheel configurations can be exploited to satisfy a body-axis control torque requirement while satisfying objectives such as minimum control energy.1-2 In general, the reaction wheel steering laws determine required torque command for each wheel in the form of matrix pseudo-inverse. In general, the attitude control command is generated in the form of a feedback control. The spacecraft body angular rate measured by gyros is used to estimate angular displacement also.⁵ Combination of the body angular rate and attitude parameters such as quaternion and MRPs(Modified Rodrigues Parameters) is typically used in synthesizing the control command which should be produced by RWs.¹ The attitude sensor signals are usually corrupted by noise; gyros tend to contain errors such as drift and random noise. The attitude determination system can estimate such errors, and provide best true signals for feedback control.⁶ Even if the attitude determination system, for instance, sophisticated algorithm such as the EKF(Extended Kalman Filter) algorithm⁶, can eliminate the errors efficiently, it is quite probable that the control command still contains noise sources. The noise and/or other high frequency components in the control command would cause the wheel speed to change in an undesirable manner. The closed-loop system, governed by the feedback control law, is also directly affected by the noise due to imperfect sensor characteristics. The noise components in the sensor signal should be mitigated so that the control command is isolated from the noise effect. This can be done by adding a filter to the sensor output or preventing rapid change in the control command. Dynamic control allocation(DCA), recently studied by Härkegård, is to distribute the control command in the sense of dynamics⁴: the allocation is made over a certain time interval, not a fixed time instant. The dynamic behavior of the control command is taken into account in the course of distributing the control command. Not only the control command requirement, but also variation of the control command over a sampling interval is included in the performance criterion to be optimized. The result is a control command in the form of a finite difference equation over the given time interval.⁴ It results in a filter dynamics by taking the previous control command into account for the synthesis of current control command. Stability of the proposed dynamic control allocation (CA) approach was proved to ensure the control command is bounded at the steady-state. In this study, we extended the results presented in Ref. 4 by adding a two-step dynamic CA term in deriving the control allocation law. Also, the strict equality constraint, between the virtual and actual control inputs, is relaxed in order to construct control command with a smooth profile. The proposed DCA technique is applied to a spacecraft attitude control problem. The sensor noise and/or irregular signals, which are existent in most of spacecraft attitude sensors, can be handled effectively by the proposed approach.

• 한국통신학회논문지
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• 제40권2호
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• pp.397-407
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• 2015

본 논문에서는 최근 스마트폰이나 웨어러블 디바이스처럼 IoT/M2M 을 위한 여러 종류의 모바일 기기에 사용되는 센서 중에서 각속도를 검출하는데 사용되는 3축 자이로스코프 센서 IC와 가속도를 검출하는데 사용되는 3축 가속도 센서IC를 1 chip으로 하는 6축 관성센서 IC를 설계하였다. 특히 본 논문에는 자이로스코프 센서의 잡음을 분석하고 이를 효과적으로 제거하기 위한 구조를 제안하였다. 자이로스코프 센서는 가속도 센서, 지자기 센서와 더불어 사용자의 동작을 인식하고, 상대적 위치를 추정하기 위한 용도로 사용되는 센서이다. 위치를 추정할 때 사용되는 센서는 아주 작은 잡음이라도 오차로 누적되기 때문에, 정확도를 높이기 위해서 저잡음 IC 설계가 아주 중요한 요소이다. 본 논문에서는 자이로스코프 센서를 모델링하고 MEMS(micro-electro-mechanical system)와 회로에서 발생하는 잡음의 주파수 특성을 분석하여 이를 효과적으로 제거하기 위한 회로 구조를 제안하였으며, 초소형, 저전력 환경에서 사용 가능하면서 잡음 수준이 아주 낮은 3축 자이로스코프 센서와 3축 가속도 센서를 포함하는 6축 1 chip IC를 제작하였다. 제작된 IC는 자이로스코프 센서 잡음의 주요 원인이 되는 quadrature error를 효과적으로 제거하기 위한 회로 구조를 사용하였고, 0.18um CMOS공정을 이용하여 0.01dps/${\sqrt{Hz}}$의 자이로스코프 센서 잡음밀도를 가지는 IC를 제작하였다.

• 센서학회지
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• 제27권1호
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• pp.31-35
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• 2018

This paper describes a low-power, SNDR (signal-to-noise and distortion ration) enhanced SAR (successive approximation register) type 12b ADC (analog-to-digital converter) with noise shaping technique. For low power consumption and small chip size of the DAC (digital-to-analog converter), the top plate sampling technique and the dummy capacitor switching technique are used to implement 12b operation with a 10b capacitor array in DAC. Noise shaping technique is applied to improve the SNDR by reducing the errors from the mismatching of DAC capacitor arrays, the errors caused by attenuation capacitor and the errors from the comparator noise. The proposed SAR ADC is designed with a $0.18{\mu}m$ CMOS process. The simulation results show that the SNDR of the SAR ADC without the noise shaping technique is 71 dB and that of the SAR ADC with the noise shaping technique is 84 dB. We can achieve the 13 dB improvement in SNDR with this noise shaping technique. The power consumption is $73.8{\mu}W$ and the FoM (figure-of-merit) is 5.2fJ/conversion-step.

• 한국지능시스템학회논문지
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• 제23권5호
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• pp.418-422
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• 2013

본 논문은 비가우시안 노이즈가 존재하는 수중환경에서 비선형 필터 기법에 따른 2차원 위치 추정에 관한 연구 내용이다. 최근 위치 추정을 위한 필터로 확장형 칼만필터(EKF: Extended Kalman filter)가 많이 사용되고 있다. 하지만, 수중과 같은 비가우시안 노이즈가 존재하는 비선형 시스템에서는 많은 문제점을 가지고 있다. 따라서 본 논문에서는 상태변이의 예측을 기반으로한 EKF를 대신하여 통계적 발생인자 에 기반을 둔 분포 재해석 기법을 이용한 2차원 파티클필터 (TDPF: Two-Dimension Particle Filter)를 제안한다. 모의 실험을 통하여 Non-Gaussian Noise 가 존재하는 수중환경에서 제안하는 TDPF의 성능을 EKF와 비교분석하였으며 TDPF가 EKF보다 정확한 위치 추정결과를 제공하는 것을 확인하였다.

• 대한전기학회:학술대회논문집
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• 대한전기학회 1998년도 추계학술대회 논문집 학회본부 C
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• pp.764-766
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• 1998

An evaluation method for oxygen permeable characteristics of the membrane covering to each cathode of multiple cathode - single anode type dissolved oxygen sensor, which has high reproducibility and is capable of measuring multiple components in solutions. For this purpose, a measuring circuit for the multiple cathode type DO sensor was designed to lower the noise signal by adapting a digital LPF to readout the sensor output accurately. Digital LPF is designed by setting up the transfer function to set the cutoff frequency to 10Hz, and the transfer function is programmed by C language, and then the filtering characteristics are evaluated with the simulation and experiments. Using this LPF added measuring circuit for the multiple cathode type DO sensor, we have obtained the calibration factor for each cathode to calibrate the variation of the output signals. The calibration factor was obtained by measuring the sensor output signal followed by oxygen partial pressure, using the same oxygen permeable membrane at each cathode of the multiple cathode type DO sensor.

• 센서학회지
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• 제14권6호
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• pp.395-401
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• 2005

A highly stable quartz crystal microbalance (QCM) that showed a stability of frequencies and exhibited a very low noise level has been developed. The long-term drift was <0.05 Hz/h over a period of 10 h, and the short-term rms (root mean square) noise was <0.015 Hz. Our QCM sensor was used as a humidity sensor employing a poly(methyl methacrylate) (PMMA) polymer film as a hygroscopic layer, which showed good characteristics in the relative humidity (RH) range of $2{\sim}90%$ RH. Comparing the characteristics of the QCM sensor with those of other types of humidity sensors employing PMMA film as a hygroscopic layer, and with other QCM sensors employing other hygroscopic layers is represented.

• 융합신호처리학회논문지
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• 제3권4호
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• pp.74-78
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• 2002

인체감지용 초전형 적외선 센서 시스템은 최소 2개 이상의 센서를 사용한다. 상부전극과 바닥전극의 디자인을 새로이 하여 센서 2개가 인체감지를 가능하게 하는 센서 시스템을 센서 1개로 구성한 변환기를 설계하였다. 초전성 효과를 나타내는 재료로는 P(VDF/TrFE) 필름을 이용하였다 제작된 적외선 센서는 기존의 2개 이상의 센서를 사용하던 시스템에 비해 거의 같은 결과인 적외선원 13 $\times$ 10$10^-6$ 에 대하여 9.62 $\times$ 10$10^5$ V/W 의 높은 전압감도를 나타내었으며 NEP (noise equivalent power) 는 3.95 $\times$ $10^-7$/ W, 그리고 specific detectivity D$^*$는 5.06 $\times$ $10^5$ cm/W나타내었다.

• 한국정밀공학회지
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• 제14권3호
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• pp.107-113
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• 1997

This paper presents the active control of a flexible cantilever beam vibration. The cantilever beam was excitied by a steady-state harmonic and white noise point force and the control was performed by one piezo ceramic actuator bonded to the surface of the beam. An adaptive controller based on filtered-x LMS algorithm was used and the controller was defined by minimizing the square of the response of error sensor. In the experiment, gap sensor was used as an error sensor while the sinusoidal or white noise was applied as a disturbance. In the case of sinusoidal input, more than 20 dB of vibration reduction was achieved over all range of the natural frequencies and it takes 5 seconds to control the vibration at first natural frequency and 1 second at other natural frequencies. In the case of white noise input, 7 dB of vibration reduction was achieved at the first natural frequency and good control performance was achieved in the considered whole frequency range. Results indicate that the vibration of a flexible cantilever beam could be controlled effectively when the piezo ceramic actuator was used with filtered-x LMS algorithm.