• 제목/요약/키워드: sensor validation

검색결과 243건 처리시간 0.029초

보안 공격에 강인한 사물인터넷 센서 기반 정보 시스템 개발 (Development of Internet of Things Sensor-based Information System Robust to Security Attack)

  • 윤준혁;김미희
    • 인터넷정보학회논문지
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    • 제23권4호
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    • pp.95-107
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    • 2022
  • 사물인터넷 센서 장치와 빅데이터 처리 기법의 개발 및 보급으로 사물인터넷 센서를 활용한 정보 시스템이 여러 산업 분야에 적용되어 활용되고 있다. 정보 시스템이 적용된 산업 분야에 따라 정보 시스템이 도출하는 정보의 정확성이 산업의 효율, 안전에 영향을 미칠 수 있다. 따라서 외부 공격으로부터 센싱 데이터를 보호하고 정보 시스템이 정확한 정보를 도출할 수 있도록 하는 보안 기법이 필수적이다. 본 논문에서는 사물인터넷 센서 기반 정보 시스템의 각 처리 단계를 대상으로 하는 보안 위협을 살펴보고, 각 보안 위협에 대한 대응 기법을 제안한다. 나아가 제안하는 대응 기법을 통합하여 보안 공격에 강인한 사물인터넷 센서 기반 정보 시스템 구조를 제시한다. 제안 시스템에서는 경량 암호 알고리즘, 난독화 기반 데이터 유효성 검사 등 경량 보안 기법을 적용함으로써 저전력, 저성능의 사물인터넷 센서 장치에서도 최소한의 처리 지연만으로 보안성을 확보할 수 있도록 한다. 보편적으로 각 보안 기법을 실제로 구현하고 실험을 통해 성능을 보임으로써 제안 시스템의 실현 가능성을 보인다.

Validation of the Atmospheric Infrared Sounder Water Vapor Retrievals Using Global Positioning System: Case Study in South Korea

  • Won, Ji-Hye;Park, Kwan-Dong;Kim, Du-Sik;Ha, Ji-Hyun
    • Journal of Astronomy and Space Sciences
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    • 제28권4호
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    • pp.291-298
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    • 2011
  • The atmospheric infrared sounder (AIRS) sensor loaded on the Aqua satellite observes the global vertical structure of atmosphere and enables verification of the water vapor distribution over the entire area of South Korea. In this study, we performed a comparative analysis of the accuracy of the total precipitable water (TPW) provided as the AIRS level 2 standard retrieval product by Jet Propulsion Laboratory (JPL) over the South Korean area using the global positioning system (GPS) TPW data. The analysis TPW for the period of one year in 2008 showed that the accuracy of the data produced by the combination of the Advanced Microwave Sounding Unit sensor with the AIRS sensor to correct the effect of clouds (AIRS-X) was higher than that of the AIRS IR-only data (AIRS-I). The annual means of the root mean square error with reference to the GPS data were 5.2 kg/$m^2$ and 4.3 kg/$m^2$ for AIRS-I and AIRS-X, respectively. The accuracy of AIRS-X was higher in summer than in winter while measurement values of AIRS-I and AIRS-X were lower than those of GPS TPW to some extent.

Autonomous hardware development for impedance-based structural health monitoring

  • Grisso, Benjamin L.;Inman, Daniel J.
    • Smart Structures and Systems
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    • 제4권3호
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    • pp.305-318
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    • 2008
  • The development of a digital signal processor based prototype is described in relation to continuing efforts for realizing a fully self-contained active sensor system utilizing impedance-based structural health monitoring. The impedance method utilizes a piezoelectric material bonded to the structure under observation to act as both an actuator and sensor. By monitoring the electrical impedance of the piezoelectric material, insights into the health of the structured can be inferred. The active sensing system detailed in this paper interrogates a structure utilizing a self-sensing actuator and a low cost impedance method. Here, all the data processing, storage, and analysis is performed at the sensor location. A wireless transmitter is used to communicate the current status of the structure. With this new low cost, field deployable impedance analyzer, reliance on traditional expensive, bulky, and power consuming impedance analyzers is no longer necessary. A complete power analysis of the prototype is performed to determine the validity of power harvesting being utilized for self-containment of the hardware. Experimental validation of the prototype on a representative structure is also performed and compared to traditional methods of damage detection.

토크센서를 이용한 CMG의 지상 시뮬레이터 개발 (Development of CMG Ground Simulator using Torque Sensor)

  • 김승현;이승목;이승우
    • 한국항공우주학회지
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    • 제37권1호
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    • pp.89-98
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    • 2009
  • CMG는 3축으로 토크를 발생시키기 위해 클러스터로 구성하여 사용할 수 있다. CMG 클러스터에서 발생되는 여러 가지 설계에 고려되어야 할 문제들이 있다. 이러한 문제들을 지상에서 미리 검증하는 것이 필수적이다. 따라서 본 논문에서 토크센서로 위성자세를 계산하는 CMG 시뮬레이터를 제안하였다. 개발과정에서 발생한 김발각문제 해결을 위해 보정방법과 칼만필터가 제시되었다. 보정방법은 계산된 김발각을 기본으로 사용하고 센서 값을 보조로 사용해서 오차를 줄인다. 또한 개발된 CMG 시뮬레이터를 이용하여 특이점 회피를 위한 구동법칙과 자세제어 로직 시험결과도 예로서 제시되었다.

더미스터 온도센서를 이용한 나노유체의 대류열전달계수 측정 장치 (Measuring Apparatus for Convective Heat Transfer Coefficient of Nanofluids Using a Thermistor Temperature Sensor)

  • 이신표
    • 대한기계학회논문집B
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    • 제40권2호
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    • pp.103-110
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    • 2016
  • 나노유체의 대류열전달 성능을 평가하는 센서로서 가는 백금 열선이 많이 사용되었다. 그러나 센서의 강도가 약해서 취급에 주의가 필요하고 측정실험에서 센서에 대한 엄밀한 교정과정을 생략하거나 정밀도 높은 기구들을 사용하지 않으면 비현실적인 대류열전달계수가 얻어졌다. 본 연구에서는 백금 열선 대신 더미스터 센서를 채택한 새로운 나노유체 대류 성능 평가장치를 제안하였고 그 작동 원리를 자세히 설명하였다. 순수 엔진오일에 대한 두 센서의 비교 실험을 통하여 더미스터 센서의 실용적 장점을 확인할 수 있었다. 제안된 장치는 개발된 나노유체의 채택 여부를 판단하는 유용한 도구로 사용될 수 있을 것이다.

The Modeling of the Differential Measurement of Air Pressure for Non-intrusive Sleep Monitoring Sensor System

  • Chee, Young-Joon;Park, Kwang-Suk
    • 대한의용생체공학회:의공학회지
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    • 제26권6호
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    • pp.373-381
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    • 2005
  • The respiratory and heart beat signals are the fundamental physiological signals for sleep monitoring in the home. Using the air mattress sensor system, the respiration and heart beat movements can be measured without any harness or sensor on the subject's body which makes long term measurement difficult and troublesome. The differential measurement technique between two air cells is adopted to enhance the sensitivity. The concept of the balancing tube between two air cells is suggested to increase the robustness against postural changes during the measurement period. With this balancing tube, the meaningful frequency range could be selected by the pneumatic filter method. The mathematical model for the air mattress and balancing tube was suggested and the validation experiments were performed for step and sinusoidal input. The results show that the balancing tube can eliminate the low frequency component between two cells effectively. This technique was applied to measure the respiration and heart beat on the bed, which shows the potential applications for sleep monitoring device in home. With the analysis of the waveform, respiration intervals and heart beat intervals were calculated and compared with the signal from conventional methods. The results show that the measurement from air mattress with balancing tube can be used for monitoring respiration and heart beat in various situations.

3축 자기장 센서 및 관성센서를 이용한 차량 방위각 추정 방법 (Vehicle Orientation Estimation by Using Magnetometer and Inertial Sensors)

  • 황윤진;최세범
    • 한국자동차공학회논문집
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    • 제24권4호
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    • pp.408-415
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    • 2016
  • The vehicle attitude and sideslip is critical information to control the vehicle to prevent from unintended motion. Many of estimation strategy use bicycle model or IMU integration, but both of them have limits on application. The main purpose of this paper is development of vehicle orientation estimator which is robust to various vehicle state and road shape. The suggested estimator use 3-axis magnetometer, yaw rate sensor and lateral acceleration sensor to estimate three Euler angles of vehicle. The estimator is composed of two individual observers: First, comparing the known magnetic field and gravity with measured value, the TRIAD algorithm calculates optimal rotational matrix when vehicle is in static or quasi-static condition. Next, merging 3-axis magnetometer with inertial sensors, the extended Kalman filter is used to estimate vehicle orientation under dynamic condition. A validation through simulation tools, Carsim and Simulink, is performed and the results show the feasibility of the suggested estimation method.

A NEW APPROACH OF CAMERA MODELING FOR LINEAR PUSHBROOM IMAGES

  • Jung, Hyung-Sup;Kang, Myung-Ho;Lee, Yong-Woong;Won, Joong-Sun
    • 대한원격탐사학회:학술대회논문집
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    • 대한원격탐사학회 2003년도 Proceedings of ACRS 2003 ISRS
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    • pp.1162-1164
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    • 2003
  • The methods of the geometric reconstruction and sensor calibration of satellite linear pushbroom images are investigated. The model of the sensor used is based on the SPOT model that is developed by Kraiky. The satellite trajectory is a Keplerian trajectory in the approximation. Four orbit parameters, longitude of the ascending node(${\omega}$), inclination of the orbit plan(I), latitude argument of the satellite(W) and distance between earth center and satellite, are used for the camera modeling. Time-dependent orbit parameters are expressed by quadratic polynomials. SPOT-5 images have been used for validation tests. The results are that the RMSE acquired from 20 GCPs is 1.763m and the RMSE of 5 checking points 2.470m. Because the ground resolution of SPOT-5 is 2.5m, the result obtained in this study has a good accuracy. It demonstrates that the sensor model developed by this study can be used to reconstruct the geometry of satellite image using pushbroom camera.

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Design and characterization of a compact array of MEMS accelerometers for geotechnical instrumentation

  • Bennett, V.;Abdoun, T.;Shantz, T.;Jang, D.;Thevanayagam, S.
    • Smart Structures and Systems
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    • 제5권6호
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    • pp.663-679
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    • 2009
  • The use of Micro-Electro-Mechanical Systems (MEMS) accelerometers in geotechnical instrumentation is relatively new but on the rise. This paper describes a new MEMS-based system for in situ deformation and vibration monitoring. The system has been developed in an effort to combine recent advances in the miniaturization of sensors and electronics with an established wireless infrastructure for on-line geotechnical monitoring. The concept is based on triaxial MEMS accelerometer measurements of static acceleration (angles relative to gravity) and dynamic accelerations. The dynamic acceleration sensitivity range provides signals proportional to vibration during earthquakes or construction activities. This MEMS-based in-place inclinometer system utilizes the measurements to obtain three-dimensional (3D) ground acceleration and permanent deformation profiles up to a depth of one hundred meters. Each sensor array or group of arrays can be connected to a wireless earth station to enable real-time monitoring as well as remote sensor configuration. This paper provides a technical assessment of MEMS-based in-place inclinometer systems for geotechnical instrumentation applications by reviewing the sensor characteristics and providing small- and full-scale laboratory calibration tests. A description and validation of recorded field data from an instrumented unstable slope in California is also presented.

Experimental Study of Spacecraft Pose Estimation Algorithm Using Vision-based Sensor

  • Hyun, Jeonghoon;Eun, Youngho;Park, Sang-Young
    • Journal of Astronomy and Space Sciences
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    • 제35권4호
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    • pp.263-277
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    • 2018
  • This paper presents a vision-based relative pose estimation algorithm and its validation through both numerical and hardware experiments. The algorithm and the hardware system were simultaneously designed considering actual experimental conditions. Two estimation techniques were utilized to estimate relative pose; one was a nonlinear least square method for initial estimation, and the other was an extended Kalman Filter for subsequent on-line estimation. A measurement model of the vision sensor and equations of motion including nonlinear perturbations were utilized in the estimation process. Numerical simulations were performed and analyzed for both the autonomous docking and formation flying scenarios. A configuration of LED-based beacons was designed to avoid measurement singularity, and its structural information was implemented in the estimation algorithm. The proposed algorithm was verified again in the experimental environment by using the Autonomous Spacecraft Test Environment for Rendezvous In proXimity (ASTERIX) facility. Additionally, a laser distance meter was added to the estimation algorithm to improve the relative position estimation accuracy. Throughout this study, the performance required for autonomous docking could be presented by confirming the change in estimation accuracy with respect to the level of measurement error. In addition, hardware experiments confirmed the effectiveness of the suggested algorithm and its applicability to actual tasks in the real world.