• Title/Summary/Keyword: Bias Stabilization

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Off-level Sampling Method for Bias Stabilization of an Electro-Optic Mach-Zehnder Modulator (전기 광학 광변조기의 바이어스 안정화를 위한 오프 레벨 샘플링 방법)

  • 양충열;홍현하;김해근
    • The Journal of Korean Institute of Communications and Information Sciences
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    • v.25 no.1B
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    • pp.42-47
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    • 2000
  • A new method for stabilizing the bias of an Electro-Optic mach-Zehnder modulator has been developed to maximize the switching extinction ratio in burst mode packet traffic. By sampling and minimizing the off-level output power of the modulator, a high extinction optical gate switch in obtain regardless of the variation of the packet traffic density.

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A study and experiment on the stabilization characteristic and the stiffness in Active Magnetic Bearing (자기베어링시스템 강성의 실험적 고찰을 통한 안정화 특성에 관한 연구)

  • 강성구;강종규;홍준희
    • Proceedings of the Korean Society of Machine Tool Engineers Conference
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    • 2004.10a
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    • pp.388-392
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    • 2004
  • Due to the lack of stiffness and difficulties of control, it is hard to achieve well balanced magnetic levitation. In this paper, we analysis the current and position stiffness change according to bias current through experiment. Then, compensation equations were presented. After obtaining PD gain for each bias current and PD gain region through levitation experiment, we consider the characteristics.

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Implementation of a Low-cost Fiber Optic Gyroscope for a Line-of-Sight Stabilization System (Line-of-Sight 안정화 시스템을 위한 저가형 광자이로스코프 구현)

  • Yoon, Yeong Gyoo;Lee, Sang-Min;Kim, Jae Hyung
    • Journal of Institute of Control, Robotics and Systems
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    • v.21 no.2
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    • pp.168-172
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    • 2015
  • In general, open-loop fiber-optic gyroscopes (FOG) are less stable than closed-loop FOGs but they offer simpler implementation. The typical operation time of line-of-sight (LOS) stabilization systems is a few seconds to one hour. In this paper, a open-loop fiber optic gyroscope (FOG) for LOS applications is designed and implemented. The design goal is aimed at implementing a low cost, compact FOG with low Angle Random Walk (ARW) (< $0.03deg/\sqrt{h}$) and bias instability (< 0.25deg/h). The FOG uses an open-loop all-fiber configuration with 100M PM fiber wound on a small diameter spool. In order to get the design goal, digital signal processing techniques for signal detection, modulation control and compensation are designed and implemented in FPGA.

Sliding Mode Attitude Control for Momentum-Biased Spacecraft

  • Bang, Hyo-Choong;Loh, Young-Hwan
    • International Journal of Aeronautical and Space Sciences
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    • v.3 no.2
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    • pp.13-23
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    • 2002
  • In this paper, we present a sliding mode control strategy for the re-orientation maneuver of rigid spacecraft containing rotating wheels. The wheels are considered as internal devices, and external inputs are employed for generation of control commands. The formulation is developed for a general case while particular example is applied to pitch bias momentum spacecraft with a single momentum wheel. The resultant control commands are used to take the gyroscopic effects into account which are caused by the rotating wheels. The controller designed demonstrates that the nutational motion of the pitch bias momentum spacecraft is effectively controlled. It is also assumed that the external control torque device is of on-off nature, and pulse width modulation technique is applied to construct proper control torque history.

Reduction of headache intensity and frequency with maxillary stabilization splint therapy in patients with temporomandibular disorders-headache comorbidity: a systematic review and meta-analysis

  • Manrriquez, Salvador L.;Robles, Kenny;Pareek, Kam;Besharati, Alireza;Enciso, Reyes
    • Journal of Dental Anesthesia and Pain Medicine
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    • v.21 no.3
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    • pp.183-205
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    • 2021
  • This systematic review and meta-analysis aimed to analyze the effectiveness of maxillary stabilization splint (SS) therapy to reduce headache (HA) intensity and HA frequency in patients with temporomandibular disorders (TMD)-HA comorbidity. Randomized controlled trials (RCTs) using full-arch coverage, hard resin, and maxillary SS therapy were included. Electronic databases, including Cochrane Library, MEDLINE through PubMed, Web of Science, and EMBASE, were searched. The risk of bias was analyzed based on Cochrane's handbook. The search yielded 247 references up to January 28, 2020. Nine RCTs were included at a high risk of bias. The comparison groups included other splints, counseling, jaw exercises, medications, neurologic treatment, and occlusal equilibration. Four studies reported a statistically significant reduction in HA intensity, and five studies reported significant improvement in HA frequency from baseline at 2-12 months in patients with TMD-HA comorbidity treated with a full-arch hard maxillary SS. HA frequency in tension-type HA (TTH) comorbid with TMD diagnoses of myofascial pain (MFP) or capsulitis/synovitis improved significantly with SS than that with full-arch maxillary non-occluding splint (NOS) in two studies. Comparison groups receiving hard partial-arch maxillary splint nociceptive trigeminal inhibition (NTI) showed statistically significant improvements in HA intensity in patients with mixed TMD phenotypes of MFP and disc displacement comorbid with "general HA." Comparison groups receiving partial-arch maxillary resilient/soft splint (Relax) showed significant improvements in both HA intensity and frequency in patients with HA concomitant with MFP. The meta-analysis showed no statistically significant difference in the improvement of pain intensity at 2-3 months with comparison of the splints (partial-arch soft [Relax], hard [NTI], and full-arch NOS) or splint use compliance at 6-12 months with comparison of the splints (partial-arch Relax and full-arch NOS) versus the SS groups in patients with various TMD-HA comorbidities. In conclusion, although SS therapy showed a statistically significant decrease in HA intensity and HA frequency when reported, the evidence quality was low due to the high bias risk and small sample size. Therefore, further studies are required.

THE VARIANCE ESTIMATORS FOR CALIBRATION ESTIMATOR IN UNIT NONRESPONSE

  • Son, Chang-Kyoon;Jung, Hun-Jo
    • Journal of applied mathematics & informatics
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    • v.9 no.2
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    • pp.869-877
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    • 2002
  • In the presence of unit nonresponse we perform the calibration estimation procedure for the population total corresponding to the levels of auxiliary information and derive the Taylor and the Jackknife variance estimators of it. We study the nonresponse bias reduction and the variance stabilization, and then show the efficiency of the Taylor and the Jackknife variance estimators by simulation study.

A CMOS Switched-Capacitor Interface Circuit for MEMS Capacitive Sensors (MEMS 용량형 센서를 위한 CMOS 스위치드-커패시터 인터페이스 회로)

  • Ju, Min-sik;Jeong, Baek-ryong;Choi, Se-young;Yang, Min-Jae;Yoon, Eun-jung;Yu, Chong-gun
    • Proceedings of the Korean Institute of Information and Commucation Sciences Conference
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    • 2014.10a
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    • pp.569-572
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    • 2014
  • This paper presents a CMOS switched-capacitor interface circuit for MEMS capacitive sensors. It consist of a capacitance to voltage converter(CVC), a second-order ${\Sigma}{\Delta}$ modulator, and a comparator. A bias circuit is also designed to supply constant bias voltages and currents. This circuit employes the correlated-double-sampling(CDS) and chopper-stabilization(CHS) techniques to reduce low-frequency noise and offset. The designed CVC has a sensitivity of 20.53mV/fF and linearity errors less than 0.036%. The duty cycle of the designed ${\Sigma}{\Delta}$ modulator output increases about 5% as the input voltage amplitude increases by 100mV. The designed interface circuit shows linearity errors less than 0.13%, and the current consumption is 0.73mA. The proposed circuit is designed in a 0.35um CMOS process with a supply voltage of 3.3V. The size of the designed chip including PADs is $1117um{\times}983um$.

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Pulse-Mode Dynamic Ron Measurement of Large-Scale High-Power AlGaN/GaN HFET

  • Kim, Minki;Park, Youngrak;Park, Junbo;Jung, Dong Yun;Jun, Chi-Hoon;Ko, Sang Choon
    • ETRI Journal
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    • v.39 no.2
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    • pp.292-299
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    • 2017
  • We propose pulse-mode dynamic $R_on$ measurement as a method for analyzing the effect of stress on large-scale high-power AlGaN/GaN HFETs. The measurements were carried out under the soft-switching condition (zero-voltage switching) and aimed to minimize the self-heating problem that exists with the conventional hard-switching measurement. The dynamic $R_on$ of the fabricated AlGaN/GaN MIS-HFETs was measured under different stabilization time conditions. To do so, the drain-gate bias is set to zero after applying the off-state stress. As the stabilization time increased from $ 0.1{\mu}s$ to 100 ms, the dynamic $R_on$ decreased from $160\Omega$ to $2\Omega$. This method will be useful in developing high-performance GaN power FETs suitable for use in high-efficiency converter/inverter topology design.

Design and Fabrication of the Receiver Section for INMARSAT-C (INMARSAT-C형 위성통신단말기의 수신단 설계 및 제작)

  • 전중성;김동일;정종혁;배정철
    • Journal of the Korea Institute of Information and Communication Engineering
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    • v.3 no.2
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    • pp.339-346
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    • 1999
  • A RF receiver section for INMARSAT-C external mounting unit was designed, fabricated and evaluated. Using a INA-03184, the high gain amplifier consists of matched amplifier type. Active bias circuitry can be used to provide temperature stability without requiring the large voltage drop or relatively high-dissipated power needed with a bias stabilization resistor. The bandpass filter was used to reduce a spurious level. As a result, the characteristics of the receiver section implemented here show 60 dB in gain, 44.83 dBc in a spurious level. The voltage standing wave ratios(VSWR)of input output port are less than 1.8:1, respectively.

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Rapid Initial Detumbling Strategy for Micro/Nanosatellite with Pitch Bias Momentum System (피치 바이어스 모멘텀 방식을 사용하는 초소형 위성의 초기 자세획득 방안 연구)

  • Lee, Byeong-Hun;Choe, Jeong-Won;Jang, Yeong-Geun;Yun, Mi-Yeon
    • Journal of the Korean Society for Aeronautical & Space Sciences
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    • v.34 no.5
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    • pp.65-73
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    • 2006
  • When a satellite separates from the launch vehicle, an initial high angular rate or a tip-off rate is generated. B-dot logic is generally used for controlling the initial tip-off rate. However, it has the disadvantage of taking a relatively long time to control the initial tip-off rate. To solve this problem, this paper suggests a new detumbling control method to be able to adapt to micro/nanosatellite with the pitch bias momentum system. Proposed detumbling method was able to control the angular rate within 20 minutes which is significantly reduced compared to conventional methods. Since the previous wheel start-up method cannot be used if the detumbling controller proposed by this paper is used, a method is also proposed for bringing up the momentum wheel speed to nominal rpm while maintaining stability in this paper. The performance of the method is compared and verified through simulation. The overall result shows much faster control time compared to the conventional methods, and achievement of the nominal wheel speed and 3-axes stabilization while maintaining stability.