• 제목/요약/키워드: gyroscope

검색결과 439건 처리시간 0.036초

Recognition of Falls and Activities of Daily Living using Tri-axial Accelerometer and Bi-axial Gyroscope

  • Park, Geun-chul;Kim, Soo-Hong;Kim, Jae-hyung;Shin, Beum-joo;Jeon, Gye-rok
    • 센서학회지
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    • 제25권2호
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    • pp.79-85
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    • 2016
  • This paper proposes a threshold-based fall recognition algorithm to discriminate between falls and activities of daily living (ADL) using a tri-axial accelerometer and a bi-axial gyroscope sensor mounted on the upper sternum. The experiment was executed ten times according to the proposed experimental protocol. The output signals of the tri-axial accelerometer and the bi-axial gyroscope were measured during eight falls and eleven ADL action sequences. The threshold values of the signal vector magnitude (SVM_Acc), angular velocity (${\omega}_{res}$), and angular variation (${\theta}_{res}$) parameter were calculated using MATLAB. From the preliminary study, three thresholds (TH1, TH2, and TH3) were set so that the falls could be distinguished from ADL. When the parameter SVM_Acc is greater than 2.5 g (TH1), ${\omega}_{res}$ is greater than 1.75 rad/s (TH2), and ${\theta}_{res}$ is greater than 0.385 rad (TH3), these action sequences are recognized as falls. If at least one or more of these conditions is not satisfied, the sequence is classified as ADL.

패키징으로 인한 응력이 MEMS 소자에 미치는 영향 분석 및 개선 (Effects of Package Induced Stress on MEMS Device and Its Improvements)

  • 좌성훈;조용철;이문철
    • 한국정밀공학회지
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    • 제22권11호
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    • pp.165-172
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    • 2005
  • In MEMS (Micro-Electro-Mechanical System), packaging induced stress or stress induced structure deformation becomes increasing concerns since it directly affects the performance of the device. In the decoupled vibratory MEMS gyroscope, the main factor that determines the yield rate is the frequency difference between the sensing and driving modes. The gyroscope, packaged using the anodic bonding at the wafer level and EMC (epoxy molding compound) molding, has a deformation of MEMS structure caused by thermal expansion mismatch. This effect results in large distribution in the frequency difference, and thereby a lower yield rate. To improve the yield rate we propose a packaged SiOG (Silicon On Glass) process technology. It uses a silicon wafer and two glass wafers to minimize the wafer warpage. Thus the warpage of the wafer is greatly reduced and the frequency difference is more uniformly distributed. In addition. in order to increase robustness of the structure against deformation caused by EMC molding, a 'crab-leg' type spring is replaced with a semi-folded spring. The results show that the frequency shift is greatly reduced after applying the semi-folded spring. Therefore we can achieve a more robust vibratory MEMS gyroscope with a higher yield rate.

비연성 수직형 마이크로 자이로스코프의 구조해석 및 최적설계 (Structural Analysis and Optimum Design of a De-coupled Vertical Micro-Gyroscope)

  • 박성균;정희문;김명훈;김형태;하성규
    • 대한기계학회논문집A
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    • 제27권11호
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    • pp.1840-1848
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    • 2003
  • This paper presents the structural analysis and optimum design of a vertical micro-gyroscope with decoupled 2 degrees of freedom (DOF), driven by electrostatic force. Simplified beam models were presented to derive the structural stiffness of the driving spring of the U shape and the sensing spring of I shape. A finite element analysis (FEA) was performed to validate each derivation. A total mass and a polar mass moment of inertia were also obtained and used in calculating the resonance frequency at each mode of the 2 DOF. The resonance frequencies of the total system were calculated using the proposed models and it has been found that they were in excellent agreement with those of the FEA. Finally, the developed analysis program was then linked to an optimum design module, and an optimum design of the micro-gyroscope was successfully performed.

표면 및 몸체 미세 가공 기술로 제작된 대기압에서 동작하는 전자력 검출형 각속도계의 연구 (A Surface-Bulk Micromachined Electromagnetic Gyroscope Operating at Atmospheric Pressure)

  • 김성혁;김용권;송진우;이장규
    • 대한전기학회:학술대회논문집
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    • 대한전기학회 2000년도 하계학술대회 논문집 C
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    • pp.2230-2232
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    • 2000
  • This paper reports an electrostatically driven and electromagnetically sensed planar vibratory gyroscope based on a surface-bulk combined micromachining. The fabricated structure has comb electrodes which are 400${\mu}m$ thick, 18${\mu}m$ wide, 600${\mu}m$ long and separated by 7${\mu}m$ so that the height-gap ratio is about 57. It also has electroplated gold springs which are 15${\mu}m$ wide, 14${\mu}m$ thick and 500${\mu}m$ long on both sides of the seismic mass. The open-loop characteristics of fabricated gyroscope at atmospheric pressure are measured on a rate table. The fabricated gyroscope has a sensitivity of 30mV/deg/sec, and a resolution of 0.1deg/sec at atmospheric pressure. It is expected that non linearity of full scale output is less than 0.8% with. the dynamic range of $\pm$500deg/sec.

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On the control of vibratory MEMS gyroscopes

  • Choura, S.;Aouni, N.;El-Borgi, S.
    • Smart Structures and Systems
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    • 제6권7호
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    • pp.793-810
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    • 2010
  • This paper addresses the control issue of vibratory MEMS-based gyroscopes. This study considers a gyroscope that can be modeled by an inner mass attached to an outer mass by four springs and four dampers. The outer mass itself is attached to the rotating frame by an equal number of springs and dampers. In order to measure the angular rate of the rotating frame, a driving force is applied to the inner mass and the Coriolis force is sensed along the y-direction associated with the outer mass. Due to micro-fabrication imperfections, including anisoelasticity and damping effects, both gyroscopes do not allow accurate measurements, and therefore, it becomes necessary to devise feedback controllers to reduce the effects of such imperfections. Given an ideal gyroscope that meets certain performance specifications, a feedback control strategy is synthesized to reduce the error dynamics between the actual and ideal gyroscopes. For a dual-mass gyroscope, it is demonstrated that the error dynamics are remarkably decreased with the application of four actuators applied to both masses in the x and y directions. It is also shown that it is possible to reduce the error dynamics with only two actuators applied to the outer mass only. Simulation results are presented to prove the efficiency of the proposed control design.

진동형 각속도계의 최적 구동신호 튜닝에 대한 연구 (A Study on the Optimal Drive Signal Tuning of Vibratory Gyroscope)

  • 이준영;전승훈;정형균;장현기;김용권
    • 대한전기학회:학술대회논문집
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    • 대한전기학회 2004년도 추계학술대회 논문집 전기물성,응용부문
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    • pp.40-42
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    • 2004
  • This paper describes a method to find an optimal driving condition of vibratory gyroscope. Mechanical coupling between driving and sensing mode degrades the performance of vibratory gyroscope. When the resonant frequencies of driving and sensing parts are fixed, frequency and amplitude of driving source affect mechanical coupling. Thus, they should be optimally tuned. To investigate the influence of driving source on mechanical coupling, we measured frequency response and displacement of driving and sensing mode using laser vibromenter. The measured frequency response and displacement show that the gyroscope has minimum mechanical coupling when the frequency of driving source is set to the intermediate value of driving and sensing part resonant frequency. Measurement also shows that the mechanical coupling increases abruptly at a certain driving voltage as the voltage increases.

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다중 질량 시스템을 이용한 자이로스코프 설계 (Design of MEMS Gyroscope Using Multi Mass System)

  • 정슨훈;이준영;정형균;장현기;김용권
    • 대한전기학회:학술대회논문집
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    • 대한전기학회 2004년도 추계학술대회 논문집 전기물성,응용부문
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    • pp.43-45
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    • 2004
  • In this paper, new design concept of MEMS gyroscope using multi mass system is proposed. The gyroscope having wide bandwidth was designed utilizing the multi mass system in order to reduce the degradation of the performance by resonance variation. The multi mass system has more than two masses and separates the resonant peak of each mass. Using MATLAB, the variation of bandwidth and driving displacement according to mass ratio of the multi mass system was analyzed. This result was compared with that of current single mass system gyroscope. In the 7 kHz resonant frequency design, the multi mass system has 395.3Hz bandwidth, which is six times larger than single mass system bandwidth, 58.5 Hz.

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진동형 마이크로 자이로스코프의 각속도 주파수 동역학적 모델의 도출 및 성능 해석 (Performance Analysis of a Vibrating Microgyroscope using Angular Rate Dynamic Model)

  • 홍윤식;이종현;김수현
    • 한국정밀공학회지
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    • 제18권1호
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    • pp.89-97
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    • 2001
  • A microgyroscope, which vibrates in two orthogonal axes on the substrate plane, is designed and fabricated. The shuttle mass of the vibrating gyroscope consists of two parts. The one is outer shuttle mass which vibrates in driving mode guided by four folded springs attached to anchors. And the other is inner shuttle mass which vibrates in driving mode as the outer frame does and also can vibrate in sensing mode guided by four folded springs attached to the outer shuttle mass. Due to the directions of vibrating mode, it is possible to fabricate the gyroscope with simplified process by using polysilicon on insulator structure. Fabrication processes of the microgyroscope are composed of anisotropic silicon etching by RIE, gas-phase etching (GPE) of the buried sacrificial oxide layer, metal electrode formation. An eletromechanical model of the vibrating microgyroscope was modeled and bandwidth characteristics of the gyroscope operates at DC 4V and AC 0.1V in a vacuum chamber of 100mtorr. The detection circuit consists of a discrete sense amplifier and a noise canceling circuit. Using the evaluated electromechanical model, an operating condition for high performance of the gyroscope is obtained.

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Gyroscope Free 관성 측정 장치를 이용한Attitude Heading Reference System 설계 (Design of Attitude Heading Reference System using Gyroscope Free Inertial Measurement Unit)

  • 손재훈;이상윤;김효석;황동환
    • Journal of Positioning, Navigation, and Timing
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    • 제13권3호
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    • pp.237-244
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    • 2024
  • An Attitude and Heading Reference System (AHRS) provides the attitude of a vehicle with a constant velocity using an Inertial Measurement Unit (IMU) and a magnetometer. In this case, in order to avoid the disadvantage of a gyroscope, an AHRS using a Gyro-Free IMU (GF-IMU) that is composed of only accelerometers may be considered instead of the gyroscopes. In this paper, a design method of an AHRS using a GF-IMU is proposed. The proposed AHRS consists of roll and pitch calculation, yaw calculation, angular acceleration and angular velocity calculation, attitude calculation, and a Kalman filter. In particular, since the angular velocity cannot be measured from a gyroscope, the angular acceleration is obtained from the accelerometer output, and the angular velocity is calculated by integrating it. In order to show the usefulness of the proposed method, a performance evaluation was carried out. The performance evaluation results show that the attitude estimation performance of the proposed AHRS is similar to that of the conventional AHRS.

진동촉각 공간 마우스 (Vibrotactile Space Mouse)

  • 박준형;최예림;이광형;백종원;장태정
    • 한국HCI학회:학술대회논문집
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    • 한국HCI학회 2008년도 학술대회 1부
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    • pp.337-341
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    • 2008
  • 본 논문에서는 핀형 진동촉각 디스플레이 장치와 자이로스코프 칩을 이용한 진동 촉각 공간 마우스를 제시한다. 이 마우스는 자이로스코프 칩을 이용하여 공중에서 동작하는 공간마우스에 본 연구실에서 자체 제작한 진동촉각 디스플레이 모듈을 통합하여 위치 입력과 진동 촉각 출력이 동시에 가능한 새로운 형식의 인터페이스 장치이다. 최근 진동촉각 디스플레이의 소형화, 저전력 소모 방향으로의 발전으로 인해 마우스나 모바일 장치 등 소형 임베디드 환경에서도 사용이 가능하게 되었다. 또한 MEMS 기술로 인한 자이로스코프나 센서 기술의 발전으로 인해 이젠 마우스 같은 소형화 제품에도 소형 자이로스코프 칩을 이용하여 평면 환경이 아닌 공간상에서 사용 가능한 마우스를 제작할 수 있게 되었다. 이 진동 촉각 마우스는 자이로스코프 칩을 이용하여 손의 동작을 인식하고 그 데이터를 블루투스 통신을 통해 PC에 전달하여 포인터를 이동시킨다. 또한 마우스와 손가락의 접촉 부위에는 $2\;{\times}\;3$의 핀형 진동촉각 디스플레이 장치가 장착되어 PC 어플리케이션 상에서 포인터 위치에 따른 흑백 이미지 정보를 제공하거나 문자를 점자로 출력시켜 주는 등 진동 촉각을 통한 정보 전달을 가능하게 해준다.

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