• 제어로봇시스템학회논문지
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• 제13권2호
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• pp.179-186
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• 2007

This paper presents new ignition method and ignition recognition logic for a microturbine. New ignition method is designed by constant speed control of a microturbine with pre-determined time during a ignition period. It make more accurate air-fuel ratio as well as give enough time to ignition system to have full performance under cold temperature. And ignition recognition logic is designed by observing output current change of inverter by generating output torque of a microturbine in the instant of ignition. For filtering a output torque current of inverter with high frequency, we applied a moving average method. So far, ignition recognition is usually implemented by measuring of exhausted gas temperature(EGT) of microturbine. The proposed logic can give more accurate judgement of ignition as well as keep a good working of starting system under out of order a temperature measuring system and biased initial value of EGT sensor. Finally, the two proposed logics are proved by field operating a microturbine under various conditions.

• 한국전기전자재료학회:학술대회논문집
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• 한국전기전자재료학회 2001년도 추계학술대회 논문집 Vol.14 No.1
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• pp.65-68
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• 2001

In the vector control methods of induction motor, the stator current is divided into the flux and torque component current. By controlling these components respectively, the methods control independently flux and torque as in the DC motor and improve the control effects. To apply the vector control methods, the position of the rotor current is identified. The indirect vector control use the parameters of the machine to identify the position of rotor flux. But due to the temperature rise during machine operation, the variation of rotor resistance degrades the vector control. To solve the problem, the q-axis is aligned to reference frame without phase difference by comparing the real flux component with the reference flux component. Then to compensate the slip, PI controller is used. The proposed method keeps a constant slip by compensating the gain of direct slip frequency when the rotor resistance of induction motor varies. To prove the validations of the proposed algorithm in the paper, computer simulations is executed.

• 한국정밀공학회지
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• 제27권7호
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• pp.109-116
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• 2010

The magnet wheel which generates on its interfacing conductive part a repulsive force and a traction torque by rotation of permanent magnets is used to manipulate the conductive plate without mechanical contact. Here, the air-gap magnetic field of the magnet wheel is shielded partially to convert the traction torque into a linear thrust force. Although a magnitude of the thrust force is constant under the fixed open region, we can change the direction of force by varying a position of the shield sheet. So, the spatial position of conductive plate is controlled by not the force magnitude from each magnet wheel but the open position of shield sheet. This paper discusses non-contact conveyance system of the conductive plate using electromagnetic forces from multiple magnet wheels.

• 한국전자통신학회논문지
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• 제13권1호
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• pp.93-100
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• 2018

본 연구는 정밀한 각속도 추종을 위해 토크오차를 보상하는 제어기와 구현에서 제어기의 안정성을 보완하는 방법을 제안한다. 또한 설계된 제어기가 점근적인 안정할 수 있음을 리아프노프 안정도이론에 근거하여 증명하였다. 제안된 제어기는 d축 기준전류를 임의 값에 대한 제어가 가능하고, 속도이득과 전류이득의 두 가지로 손쉽게 제어성능을 달성할 수 있도록 하였다. 약 750W급의 IPMSM에 적용한 결과 레퍼런스 속도 1200[RPM]에 대한 정상상태 오차는 0.1[%]이내이며, 약 5[Nm]의 상수부하에서 약 0.2초 이내에 외란을 극복하여 점근적인 안정한 제어기임을 확인 할 수 있다.

• 대한전기학회논문지
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• 제40권2호
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• pp.162-172
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• 1991

In proportion to the capacity enlargement of the induction motor system controlled by current source inverter, the capacitance of the commutating capacitor is enlarged and then the spike value of output voltage is increased at the moment of charge and discharge. Moreover, the output currnet includes a number of harmonic components. Such voltage spike and harmonics generate the torque ripple and lead to bad effects on the performance of the induction motor. In this study, all the harmonics excluding 17th and 19th harmonics were mostly elimunated by adopting 18-phase Triple High Frequency Current Source Inverter(HFCSI), and the spike component of output voltage was reduced by adding the Voltage Clamping Circuit(VCC). As a result, the torque ripple and the commutation loss were reduced and the performance of the system was improved. Experiments for speed control were carried out in the tripple current source inverter system for induction motor drive. Overall system was controlled by ONE CHIP MICROCOMPUTER(INTEL 8751). Control circuits were simplified and good experimental results in the constant V/F control were obtained due to the flexibility of the microcomputer.

• 대한전기학회:학술대회논문집
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• 대한전기학회 2007년도 제38회 하계학술대회
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• pp.1043-1044
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• 2007

The line-start permanent magnet synchronous motor has a high efficiency and an advantage in constant speed operation regardless of the effect of load variation. However it is difficult to predict the performance of characteristics accurately, because of the unbalanced starting torque with the initial starting position of the rotor and the generation of a break torque. In this paper the dynamic characteristics of the line-start permanent magnet synchronous motor are described and compared with those of the squirrel-cage induction motor through the simulation to find the characteristics of the permanent magnets and the rotor bars in the line-start permanent magnet synchronous motor. Finally this paper gives the comparison between the simulation results and the experiment results.

• 로봇학회논문지
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• 제18권3호
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• pp.299-307
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• 2023

In the midst of accelerating wars around the world, unmanned robot technology that can guarantee the safety of human life is emerging. ERP-42 is a modular platform that can be used according to the application. In the field of defense, it can be used for transporting supplies, reconnaissance and surveillance, and medical evacuation in conflict areas. Due to the nature of the military environment, atypical environments are predominant, and in such environments, the platform's path followability is an important part of mission performance. This paper focuses on reducing the minimum turning radius in terms of improving path followability. The minimum turning radius of the existing 2WS/2WD in-wheel platform was reduced by increasing the torque of the independent driving in-wheel motor on the rear wheel to generate oversteer. To determine the degree of oversteer, two GPS were attached to the center of the front and rear wheelbases and measured. A closed-loop speed control method was used to maintain a constant rotational speed of each wheel despite changes in load or torque.

• Wind and Structures
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• 제19권1호
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• pp.1-14
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• 2014

Rail-mounted cranes can be easily damaged by a sudden gust of wind while working at a running speed, due to the large mass and high barycenter positions. In current designs, working rail-mounted cranes mainly depend on wheel braking torques to resist large wind load. Regular brakes, however, cannot satisfactorily stop the crane, which induces safety issues of cranes and hence leads to frequent crane accidents, especially in sudden gusts of wind. Therefore, it is necessary and important to study the braking performance of working rail mounted cranes under wind load. In this study, a simplified mechanical model was built to simulate the working rail mounted gantry crane, and dynamic analysis of the model was carried out to deduce braking performance equations that reflect the qualitative relations among braking time, braking distance, wind load, and braking torque. It was shown that, under constant braking torque, there existed inflection points on the curves of braking time and distance versus windforce. Both the braking time and the distance increased sharply when wind load exceeded the inflection point value, referred to as the threshold windforce. The braking performance of a 300 ton shipbuilding gantry crane was modeled and analyzed using multibody dynamics software ADAMS. The simulation results were fitted by quadratic curves to show the changes of braking time and distance versus windforce under various mount of braking torques. The threshold windforce could be obtained theoretically by taking derivative of fitted curves. Based on the fitted functional relationship between threshold windforce and braking torque, theoretical basis are provided to ensure a safe and rational design for crane wind-resistant braking systems.

• 전력전자학회논문지
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• 제12권4호
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• pp.291-299
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• 2007

영구자석 동기전동기를 단위 전류 당 최대 토크 운전 점에서 운전하기 위해서는 전동기의 상전류 및 온도에 따라 변화하는 인덕턴스 및 역기전력 상수와 같은 전동기의 파라미터들에 대한 정확한 값을 알고 있어야 한다. 전동기 파라미터의 온라인 추정을 위한 적응 추정 기법은 정확한 값을 추정하는 데 어려움이 있고 복잡한 수학 연산을 필요로 하기 때문에 실질적인 응용에는 적합하지 못하다. 본 논문의 목적은 느린 동적 부하를 가지는 벡터 제어 영구자석 동기전동기 구동장치를 위한 단순한 단위 전류 당 최대 토크 운전 점 추적 제어 전략을 제안하는 것이다. 제안된 방식은 전류 위상각을 조절하고 지령 전력의 변화를 관측함으로써 단위 전류 당 최대 토크 운전 점들을 찾아간다. 전류 위상각 조절 전략은 부하 변동이 지령 전력에 미치는 영향을 감지할 수 있도록 설계된다. 따라서, 제안된 방식은 부하 변동에 관계없이 영구자석 동기전동기의 단위 전류 당 최대 토크 운전 점들을 추적할 수 있다. 컴퓨터 시뮬레이션과 실험을 통하여 제안된 방식의 효용성을 보인다.

• 농업과학연구
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• 제11권1호
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• pp.160-175
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• 1984

로우터리 경운(耕耘)날의 회전속도(回轉速度) 및 작업속도(作業速度)가 경운소요(耕耘所要)토오크에 미치는 영향을 분석(分析)하기 위(爲)하여, 형상각(形狀角) ${\theta}=30^{\circ}$, $40^{\circ}$인 2종(種)의 경운(耕耘)날로 로우터리축(軸)을 204, 243, 285, 360rpm 4단계로, 전진속도(前進速度)는 29.40cm/s, 46.93cm/s로 변화(變化)시키면서 인공토양조(人工土壤槽)에서 dynamic strain gage system을 이용(利用)하여 경운소요(耕耘所要)토오크를 측정분석(測定分析)한 결과(結果)를 요약(要約)하면 다음과 같다. 1. 경운(耕耘)날의 회전속도(回轉速度) 및 전진속도(前進速度)는 경운소요(耕耘所要)토오크에 교호작용(交互作用)으로 영향(影響)을 미치는 것으로 분석(分析)되었으며, response surface analysis를 통(通)하여 분석(分析)한 수학적(數學的)인 모형(模型)은 다음과 같다. $$T=a_0+a_1V+a_2R+a_3VR+a_4VR^2$$ 여기서 T=경운소요(耕耘所要)토오크 (kg-m) $a_0$=당(當)수(數) $a_1,\;a_2,\;a_3,\;a_4$= 계(係)수(數) V=경운장치(耕耘裝置)의 전진속도(前進速度) (cm/s) R=경운(耕耘)날의 회전속도(回轉速度) (rpm) 2. 최대경운소요(最大耕耘所要)토오크는 로우터리날 회전속도(回轉速度)가 증가(增加)함에 따라 ${\frac{{\partial}T}{{\partial}V}}$는 증가(增加)하였으며, 200~220rpm에서 증가율(增加率)이 최저(最低)가 되었고, 같은 조건(條件)에서 ${\frac{{\partial}T}{{\partial}R}}$은 감소(減少)하는 경향(傾向)이었으며, 전진속도(前進速度)가 증가(增加)함에 따라 감소율(減少率)은 증가(增加)되었다. 3. 평균경운소요(平均耕耘所要)토오크는 회전속도(回轉速度)가 320~360rpm에서 ${\frac{{\partial}T}{{\partial}R}}$의 變化가 적었으며, ${\frac{{\partial}T}{{\partial}R}}$은 회전속도(回轉速度)가 증가(增加)함에 따라 감소율(減少率)이 증가(增加)되었다. 4. 전진속도(前進速度)에 대(對)한 토양(土壤)의 단위체적당(單位體積當) 평균경운소요(平均耕耘所要)토오크의 변화율(變化率)${\frac{{\partial}T}{{\partial}R}}$는 270~300rpm에서 최저(最低)가 되었으며, ${\frac{{\partial}T}{{\partial}R}}$은 V=29.40cm/s와 V=46.93cm/s일때 변화율(變化率)이 280~290rpm에서 교착(交錯)하였다. 5. 로우터리날의 형상각(形狀角)이 증가(增加)함에 따라 순경운소요동력(純耕耘所要動力)은 증가(增加)하였다. 그러나 실제(實際) 이용면(利用面)에서는 형상각(形狀角)이 작으면 로우터리날에 검불이 감기게 되므로 소요동력(所要動力)이 크게 증가(增加)함을 보여주는 연구결과도 있다. 그러므로 형상각(形狀角) 변화(變化)에 대(對)해서는 계속 연구(硏究)되어야 할 과제(課題)라 인정(認定)된다.