• 제목/요약/키워드: Reference Accelerometer

검색결과 63건 처리시간 0.023초

기준 가속도계를 이용한 보의 면내 진동인덴시티 측정 (Measurements of the In-Plane Vibration Intensity of a Beam Using an Reference Accelerometer)

  • Kim, C. R.;H. G. Kil;J. S. Jeon;S. Y. Hong
    • 한국소음진동공학회:학술대회논문집
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    • 한국소음진동공학회 2002년도 추계학술대회논문초록집
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    • pp.383.2-383
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    • 2002
  • In this paper, an experimental technique using a reference accelerometer has been developed to measure the in-plane vibration intensity of a beam. It has the advantages of shortening measurement time and reducing accelerometer phase error comparing with the cross spectral Intensity measurement technique using an accelerometer array. The distribution of the in-plane vibration Intensity over the beam has been measured. (omitted)

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기준 가속도계를 이용한 보의 면내 진동인텐시티 측정 (Measurements of the In-Plane Vibration Intensity of a Beam Using an Reference Accelerometer)

  • 김창렬;길현권;전진숙;홍석윤
    • 한국소음진동공학회:학술대회논문집
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    • 한국소음진동공학회 2002년도 추계학술대회논문집
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    • pp.848-851
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    • 2002
  • In this paper, an experimental method using a reference accelerometer has been developed to measure the in-plane vibration intensity of a beam. It has the advantages of reducing accelerometer phase error comparing with the cross spectral intensity measurement technique using an accelerometer array. It needs no measurement of the input force required in the frequency response method using the only one accelerometer This method has been used to measure the in-plane vibration intensity over the beam. The result has been compared with an input power and the vibration intensity obtained with other methods. It showed that the present experimental method can be effectively used to measure the structural in-plane vibration intensity.

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감쇠 단을 갖는 보의 면내 진동인텐시티 측정에 관한 연구 (Study on Measurements of the In-Plane Vibration Intensity In a Beam With a Damped End)

  • 김창열;길현권;홍석윤
    • 한국음향학회지
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    • 제24권7호
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    • pp.371-378
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    • 2005
  • 본 연구에서는 면내 진동하는 감쇠 단을 갖는 보에서 진동파워의 크기와 방향을 나타내는 면내 진동인텐시티를 측정하였다. 보의 면내 진동인텐시티 측정 방법으로서 3가지 다양한 방법을 적용하였다. 이러한 방법들은 2개의 가속도계 선형 배열을 이용하는 가속도계배열법과 하나의 가속도계를 갖고 주파수응답함수를 이용하는 주파수응답함수법 그리고 기준 가속도를 고정시키고 다른 하나의 가속도계를 이용하는 기준가속도계법 들이다. 본 연구에서는 이러한 방법들을 적용하여 보의 진동인텐시티 공간 분포를 측정하여 비교하였으며, 또한 가진 점에서 주어지는 입력 파워와 비교를 통하여 적용 가능성을 확인하였다. 이러한 결과들로부터 보의 면내 진동인텐시티를 측정하기 위하여 가속도계배열법뿐만이 아니라 주파수응답함수법과 기준가속도계법 또한 효과적으로 사용될 수 있음을 보였다.

스트랩다운 비행자세(롤, 피치)측정장치의 가속도계 보조 혼합알고리즘 (An accelerometer aided mixing algorithm for strapdown attitude(roll, pitch) reference system)

  • 유재종;이장규
    • 제어로봇시스템학회:학술대회논문집
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    • 제어로봇시스템학회 1989년도 한국자동제어학술회의논문집; Seoul, Korea; 27-28 Oct. 1989
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    • pp.54-58
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    • 1989
  • The purpose of this paper is to develop a more accurate attitude algorithm with low grade gyro output. The proposed algorithm estimates attitudes by combining accelerometer and gyro output. For performance improvement of the algorithm, a method of velocity compensation is proposed for a better attitude estimation which is calculated from the accelerometer output. Velocity compensation is done by using Kalman Filter to estimate another velocity component.

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혼합정합 전달정렬시 해상항체의 가관측성 향상조건에 관한 연구 (A study of observability enhancement by matching methods at sea)

  • 김경주;고영웅;박찬웅
    • 제어로봇시스템학회:학술대회논문집
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    • 제어로봇시스템학회 1996년도 한국자동제어학술회의논문집(국내학술편); 포항공과대학교, 포항; 24-26 Oct. 1996
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    • pp.867-870
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    • 1996
  • Often an INS has to be aligned in navigation. In these cases it is necessary to obtain some reference information on the state of the aligned INS(Slave) such as its position, its velocity of its angular rate. Usually the reference information is velocity which is supplied by another reference INS. In the alignment state the velocity computed by the reference INS(Master) is compared with that computed by the slave INS and the difference which is indicative of the slave misalignment with respect to the master, is processed by a Kalman filter which estimates misalignment as well as the slave gyro and accelerometer error states. The operation of aligning a slave INS with a master INS comparing quantities computed by both INS is known as transfer alignment. The delivery vehicle performs error these maneuvers enable the TA Kalman filter to separate between the tilt errors and the accelerometer biases which otherwise are unobservable. The basic objective this paper is to study the observability enhancement by ship's maneuvering and matching methods during transfer alignment at sea.

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Golf Green Slope Estimation Using a Cross Laser Structured Light System and an Accelerometer

  • Pham, Duy Duong;Dang, Quoc Khanh;Suh, Young Soo
    • Journal of Electrical Engineering and Technology
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    • 제11권2호
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    • pp.508-518
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    • 2016
  • In this paper, we propose a method combining an accelerometer with a cross structured light system to estimate the golf green slope. The cross-line laser provides two laser planes whose functions are computed with respect to the camera coordinate frame using a least square optimization. By capturing the projections of the cross-line laser on the golf slope in a static pose using a camera, two 3D curves’ functions are approximated as high order polynomials corresponding to the camera coordinate frame. Curves’ functions are then expressed in the world coordinate frame utilizing a rotation matrix that is estimated based on the accelerometer’s output. The curves provide some important information of the green such as the height and the slope’s angle. The curves estimation accuracy is verified via some experiments which use OptiTrack camera system as a ground-truth reference.

고충격 미소가속도계의 압저항-구조 연성해석 및 최적설계 (Piezoresistive-Structural Coupled-Field Analysis and Optimal Design for a High Impact Microaccelerometer)

  • 한정삼;권순재;고종수;한기호;박효환;이장우
    • 한국군사과학기술학회지
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    • 제14권1호
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    • pp.132-138
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    • 2011
  • A micromachined silicon accelerometer capable of surviving and detecting very high accelerations(up to 200,000 times the gravitational acceleration) is necessary for a high impact accelerometer for earth-penetration weapons applications. We adopted as a reference model a piezoresistive type silicon micromachined high-shock accelerometer with a bonded hinge structure and performed structural analyses such as stress, modal, and transient dynamic responses and sensor sensitivity simulation for the selected device using piezoresistive-structural coupled-field analysis. In addition, structural optimization was introduced to improve the performances of the accelerometer against the initial design of the reference model. The design objective here was to maximize the sensor sensitivity subject to a set of design constraints on the impact endurance of the structure, dynamic characteristics, the fundamental frequency and the transverse sensitivities by changing the dimensions of the width, sensing beams, and hinges which have significant effects on the performances. Through the optimization, we could increase the sensor sensitivity by more than 70% from the initial value of $0.267{\mu}V/G$ satisfying all the imposed design constraints. The suggested simulation and optimization have been proved very successful to design high impact microaccelerometers and therefore can be easily applied to develop and improve other piezoresistive type sensors and actuators.

심박수 적응형 심박 조율 알고리즘 설계 및 평가: 시뮬레이션 연구 (Design and Evaluation of Blending Algorithm for Rate Adaptive Pace: Simulation Study)

  • 명현석;이경중
    • 대한의용생체공학회:의공학회지
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    • 제40권1호
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    • pp.32-37
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    • 2019
  • In this study, we designed a blending algorithm for rate adaptive pacing for cardiac pacemaker. Generally, rate adaptive pacing (RAP) is applied to patients whose heart rate does not rise during exercise for chronotropic incompetence (CI) patient. It is very important to develop an algorithm for RAP that can be properly applied to CI patients. In order to design an RAP algorithm we used dual sensors. Firstly, we designed a bio-signal measurement system based on the dual sensors, which are accelerometer and respiratory system. Secondly, we conducted treadmill test for the simulation experiment while using 3-lead ECG as reference. Finally, we designed a blending algorithm based on activation state of the dual sensors. The proposed blending algorithm was subdivided into three sections based on the accelerometer signal, which are rapidly increased section (W1), hardly changed section (W2), and decreased section (W3). Each weight is set aside for each section. To evaluate this algorithm, ten healthy adult males were participated. The correlation and Root Mean Square Error between the proposed algorithm and the reference were compared, and shown to be r=0.88 and 2.82 bpm, respectively. These results show that the proposed blending algorithm of dual sensors enables proper tracking of the heart rate during exercise. Also, it shows the possibility that the proposed blending algorithm can be applied to improve quality of life of the chronotropic incompetence patient.

MEMS형 가속도 센서를 이용한 지진 데이터 취득 시스템의 설계 및 구현 (Design and Implementation of Seismic Data Acquisition System using MEMS Accelerometer)

  • 최훈;배현덕
    • 전기학회논문지
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    • 제61권6호
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    • pp.851-858
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    • 2012
  • In this paper, we design a seismic data acquisition system(SDAS) and implement it. This system is essential for development of a noble local earthquake disaster preventing system in population center. In the system, we choose a proper MEMS-type triaxial accelerometer as a sensor, and FPGA and ARM processor are used for implementing the system. In the SDAS, each module is realized by Verilog HDL and C Language. We carry out the ModelSim simulation to verify the performances of important modules. The simulation results show that the FPGA-based data acquisition module can guarantee an accurate time-synchronization for the measured data from each axis sensor. Moreover, the FPGA-ARM based embedded technology in system hardware design can reduce the system cost by the integration of data logger, communication sever, and facility control system. To evaluate the data acquisition performance of the SDAS, we perform experiments for real seismic signals with the exciter. Performances comparison between the acquired data of the SDAS and the reference sensor shows that the data acquisition performance of the SDAS is valid.

A Gyro-Free INS Algorithm in the Navigation Frame and Its Application to the Spinning Vehicle with High Rotation Rate

  • Lee, Junhak;Kim, Heyone;Oh, Sang Heon;Do, Jae Chul;Nam, Chang Woo;Hwang, Dong-Hwan;Lee, Sang Jeong
    • Journal of Positioning, Navigation, and Timing
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    • 제7권2호
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    • pp.91-103
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    • 2018
  • Conventional inertial measurement units cannot be used in the spinning vehicle with high rotation rate due to gyro's narrow operation range. By the way, angular acceleration can be measured using the accelerometer array distributed in the vehicle. This paper derives a mechanization for the gyro-free INS in the navigation frame, and proposes a gyro-free INS algorithm based on the derived mechanization. In addition, the proposed algorithm is used to estimate angular velocity, attitude, velocity, and position of a spinning vehicle with high rotation rate. A MATLAB-based software platform is configured in order to show validation of the proposed algorithm. The reference trajectory of a spinning vehicle at 3 round per second, 30 round per second are set up, and the outputs of accelerometer are generated when triads of accelerometer are located at the origin and all the axes. Navigation results of the proposed algorithm for the generated output are presented. The results show that the proposed navigation algorithm can be applied to the spinning vehicle with high rotation rate.