• Journal of the Korean Society of Propulsion Engineers
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• v.22 no.6
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• pp.28-36
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• 2018

A study was conducted to apply open-loop control to the combustion instability in a dump combustor using gaseous hydrocarbon fuels. Control power and frequency were varied by employing a loudspeaker under combustion conditions with similar characteristic chemistry times of the fuels. In the case of open-loop control where the frequency was identical to the combustion instability frequency, the open-loop control power affected the control performance. Results obtained from conducted open-loop control tests, where the frequency was different from the combustion instability frequency, show that setting the open-loop control frequency similar to the combustion instability frequency is effective.

• Proceedings of the KIPE Conference
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• 2015.07a
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• pp.405-406
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• 2015

높은 동작 주파수를 가지는 LLC 공진형 컨버터는 수동 소자들의 사이즈가 작아져 전력밀도가 증가하는 장점이 있다. 하지만 높은 전력 밀도를 구현하기 위한 작은 수동 소자들은 컨버터 개루프 이득을 변동시키고 기존의 피드백 제어기를 사용할 경우 불안정한 동작을 가진다. 따라서 적절한 위상 및 이득 여유을 가지는 루프 이득을 구현하기 위하여 작은 수동 소자 사용에 따른 개루프 이득을 분석하여 적절한 피드백 제어기를 설계한다. 본 논문은 500 kHz의 동작 주파수를 가지는 LLC 공진형 컨버터를 설계 및 제작하고 수동 소자의 크기에 따른 소신호를 분석한다. 이를 바탕으로 적절한 제어기를 설계하고 안정한 동작을 검증하였다.

• 대한공업교육학회지
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• v.31 no.2
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• pp.364-380
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• 2006

This paper presents a procedure for designing command to maneuver flexible structure with very little residual vibration, even in the presence of modeling errors. For the open loop maneuver, the various shaped profiles using multiple step inputs delayed in time are considered for robustness and compared with the responses of rigid body and flexible body in virtue of simulations and experiments. Input shaping generates vibration-reducing shaped commands through convolution of an impulse sequence with the desired command. A flexible model with a cylindrical hub and four symmetric appendages is considered to examine the responses to real plant, and to illustrate the effectiveness of the proposed shapers. The appendages are long and flexible, leading to low frequency vibration under any control action. It is shown by a series of simulation that a properly designed feedback controller with input shaper performs well, as compared with open loop controller with input shaper. The control objective is to achieve a fast settling time of residual vibration to flexible structure and robustness (insensitivity)to plant uncertainty, to eliminate residual vibration.

• The Journal of Korean Institute of Electromagnetic Engineering and Science
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• v.20 no.6
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• pp.570-579
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• 2009

In this paper, we presented a Vt-DRO with a wide electrical frequency tuning range, using open-loop gain method. The Vt-DRO was composed of 3-stages, resonator, amplifier and phase shifter. In order to satisfy an oscillation condition, we determined magnitude and phase of each stage. The measured S-parameter of cascaded 3-stages shows open-loop oscillation condition. Also, using measured open loop group delay, we derived the relation for electrical frequency tuning range. The Vt-DRO was implemented by connecting the input and the output of the designed open-loop and resulted in closed-loop. As a results, tuning-range of Vt-DRO is 82 MHz, which is close to the predicted results for tuning voltage 0${\sim}$10 V and shows linear frequency tuning at the center frequency of 5.3 GHz. The phase noise is -104 ${\pm}$1 dBc/Hz at 100 kHz offset frequency and power is 5.86${\pm}$1 dBm respectively.

• Journal of the Korea Institute of Military Science and Technology
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• v.11 no.3
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• pp.5-12
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• 2008

This paper presents the features of an impact angle constrained open-loop optimal trajectory which is given by a function of initial conditions and optimal guidance gains. Using missile motion described by linearized kinematic equations and a proper form of performance index, an inverse optimal problem is suggested to investigate the gains related to the performance index. The flight trajectory and time-to-go can be shaped in terms of the optimal guidance gains. The results are evaluated by 3-DOF simulation.

• Proceedings of the KIEE Conference
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• 1998.07a
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• pp.205-208
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• 1998

영구자석형 하이브리드 스텝모터는 저가이며 개루프 제어 장치와 더불어 기계적인 제어시스템분야에서 광범위하게 이용되어 왔다. 서보모터 기술의 발달에 따라 영구자석형 스템모터는 고토크, 정밀제어의 응용분야에 있어 중요한 위치를 계속 점유하고 있다. 스텝모터는 외란으로서 작용하는 부하의 영향에 대해 안정한 견고성을 가지며, 적당한 속도와 양호한 분해능의 조합으로 신뢰도가 높고, 구조상 단순한 특징을 갖고 있다. 최근 저가의 개루프 위치제어 장치에 2상 스텝모터와 5상 스텝모터 중에서 어느 것이 더 적합한가에 대한 기술적인 주제가 주목할 어느 것이 더 적합한가에 대한 기술적인 주제가 주목할 만한 문제로 대두되고 있다. 이 두 기기의 구조는 거의 유사하며 같은 원리로 동작한다. 본 논문에서는 이 두 기기의 동작이 명백히 비교될 수 있는 기본적인 수준으로 돌아가서 두 모델을 고찰했다.

• ICROS
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• v.17 no.1
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• pp.31-38
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• 2011

주파수 영역에서 제어기를 설계하기 위해서는 시스템의 대역폭, 초대 주파수 응답, 저주파에서의 이득, 고주파에서의 이득 감쇄 정도를 고려한다. 또한 나이퀴스트 선도, 보우드 선도 등을 활용하여 폐루프 제어 시스템의 이득여유, 위상 여유를 확보할 수 있도록 한다. 일반적으로 저주파 영역에서는 개루프의 이득이 기준치보다 크도록 하고, 고주파수 영역에서는 기준치보다 작도록 설계를 하며, 폐루프 응답에서 대역폭이 유지되고, 공진피크점의 응답 크기는 1에 비하여 과도하게 크지 않도록 설계를 한다.

• Journal of the Korean Society for Aeronautical & Space Sciences
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• v.43 no.11
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• pp.998-1007
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• 2015

The $H_{\infty}$ control theory using LMI method is applied to design an attitude controller of radial type satellite that has strongly coupled channels due to the large product of inertia. It is observed that the cross-over frequency of open-loop with $H_{\infty}$ controller is lower than that of open-loop without controller, which is not typical phenomenon in an optimal control design result: it is interpreted that due to a large product of inertia, there is certain limit in increasing agility of satellite by just tuning weighting function. ${\mu}$-analysis is performed to verify the stability and performance robustness with the assumption of +/-5% MOI variation. ${\mu}$-analysis result shows that the variation of principal MOI degrades the stability and performance robustness more than the variation of POI does.

• KIPS Transactions on Computer and Communication Systems
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• v.11 no.8
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• pp.241-248
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• 2022

In this paper, the PID controller and Kalman filter are applied to improve the automobile cruise control in the environment with disturbance and noise, and the performance is verified through diverse simulation. First, a mathematical model for a automobile cruise control system is introduced. Second, the performance degradation due to disturbance in the basic open-loop control based cruise control system is shown and then PID controller-based feedback control system to resolve this problem is verified. Third, to improve the performance degradation due to sensor noise that may occur during the feedback process, a Kalman filter is applied and verified. Ultimately, it is verified that the designed cruise control system with PID controller and Kalman filter not only satisfies all performance conditions but also has the ability for disturbance rejection and noise reduction.

• Journal of Institute of Control, Robotics and Systems
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• v.10 no.8
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• pp.669-672
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• 2004

This paper considers the implementation and experiments of an open-loop Cylindrical Vibratory Gyroscope(CGV). An open-loop CGV composed of thin cylindrical vibrating element, electromagnetic drive and pick-off element with open-loop control was designed and fabricated. The experimental performance tests of the open-loop CGV were done using a temperature chambered rate table. Also, the limitations of open-loop CGV were analyzed and the solution for the limitations was proposed.