• 제목/요약/키워드: 2-axis control

검색결과 728건 처리시간 0.039초

단축조종 고속회전 유도탄의 비례항법유도 및 오차해석 (Proportional navigation guidance and error analysis of fast-rolling single-axis control missiles)

  • 전병을;송찬호
    • 제어로봇시스템학회:학술대회논문집
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    • 제어로봇시스템학회 1996년도 한국자동제어학술회의논문집(국내학술편); 포항공과대학교, 포항; 24-26 Oct. 1996
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    • pp.482-485
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    • 1996
  • We design a homing guidance law based on the proportional navigation for the fast-rolling, single-axis control missiles and analyse the misdistance of the designed guidance system. The guidance law includes a compensation scheme which compensates for the phase-shift between the commanded and achieved acceleration which is peculiar to the fast rolling airframe with single-axis control. In the error analysis of the guidance system, we calculate the misdistance with respect to the target maneuver on the 3-dimensional space via direct simulations. Also, we conduct adjoint simulation on the 2-dimensional plane in case that phase-shift is perfectly compensated. Finally we approximate the linear time-varying dynamics of the missile with autopilot to a linear time-invarient system, and as a result we can find the misdistance as a closed-form.

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T-Scan system을 이용한 측두하악 장애 환자의 교합 분석에 관한 연구 (OCCLUSAL ANALYSIS OF PATIENTS WITH TEMPOROMANDIBULAR DYSFUNCTION BY USE OF T-SCAN SYSTEM)

  • 박선주;정재헌
    • 대한치과보철학회지
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    • 제29권3호
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    • pp.121-140
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    • 1991
  • Fifteen dental college students of Chosun University without the abnormal occlusion, the history and symptom of temporomandibular dysfunction(TMD), and who had all permanent teeth except third molar and the fifteen moderate group and the fifteen severe group classified according to Helkimo's dysfunction index among patients on the basis of the symptom of TMD were selected. The occlusal contact, occlusal force and occlusal interference in eccentric movement was studied and analyzed using T-Scan system. The result were as follows : 1. The TLR centering around midsagittal axis was located at $1.42{\pm}0.82mm$ in control group, $3.36{\pm}1.45mm$ in severe group, and as TMD was heavier, occlusal contact was located at the farther point from midsagittal axis. 2. The PLR from the first contact to the fifth contact centering around midsagittal axis was located at $1.73{\pm}1.78mm$ in control group, $3.36{\pm}1.41mm$ in moderate group, and $5.39{\pm}4.32mm$ in severe group, and as TMD was heavier, occlusal contact was located at the farther point from midsgittal axis. 3. The TFB, PFB, RFB and LFB of occlusal contact centering around incisal axis had no significant difference statistically among control group, moderate group, and severe group, and it was located at first molar. 4.The LF and RF was smaller in TMD group than in control group. 5. The LR moment of occlusal force centering around midsagittal axis was located at $178.51{\pm}139.81N.mm$ in control group, $466.25{\pm}296.47N.mm$ in moderate group, and $749.18{\pm}588.18N.mm$ in severe group. And as TMD was heavier, it was located at the farther point from midsagittal axis. 6. The RL and LL of occlusal force centering around incisal axis had not-significance statistically among control group, moderate group, and severe group, and it was at the first molar. 7. The number of occlusal interference of the eccentric movement was increased in the patients of TMD.

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2축 윤곽제어를 위한 소프트웨어 보간자 개발에 관한 연구 (Development of Software Interpolator for Two-Axis Contouring Control)

  • 김교형;이기설
    • 대한기계학회논문집
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    • 제12권2호
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    • pp.389-396
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    • 1988
  • 본 연구에서는 위의 세가지 보간 알고리즘 가운데서 가장 속도의 균일성이 좋은 DDA방식을 채택하였다. 그리고 윤곽제어에서 가공경로는 대개 직선과 원호 구간의 조합으로 구성되어질 수 있기 때문에, 본 연구에서는 직선 및 원호보간만 고려하기로 한다.

Stability Comparison of New Simplified Speed Sensorless Vector Control Systems for Induction Motors

  • Mangindaan, Glanny M.Ch.;Tsuji, Mineo;Hamasaki, Sin-Ichi
    • Journal of international Conference on Electrical Machines and Systems
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    • 제3권2호
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    • pp.126-131
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    • 2014
  • This paper discusses stability of new simplified sensorless vector control systems of induction motors (IM). The simplified sensorless systems estimate the flux angle by using the output voltage of d-axis PI current controller to achieve the q-axis flux zero. Two simplified sensorless systems are studied. The difference of two systems is the presence or absence of a q-axis PI current controller. The systems stability is compared by deriving linear state equations and showing root loci and unstable regions. Furthermore, transient responses and experiment results make clear the stability of the proposed system.

An Integrated Approach to the Analysis and Design of a Three-Axis Cross-Coupling Control System

  • Jee, Sung-Chul;Lee, Hak-Chul
    • International Journal of Precision Engineering and Manufacturing
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    • 제8권2호
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    • pp.59-63
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    • 2007
  • We propose a controller design analysis for a cross-coupling control system, which is essential for achieving high contouring accuracy in multi-axis CNC systems. The proposed analysis combines three axial controllers for each individual feed drive system together with a cross-coupling controller at the beginning of the design stage in an integrated manner. These two types of controllers used to be separately designed and analyzed since they have different control objectives. The proposed scheme is based on a mathematical formulation of a three-dimensional contour error model and includes a stability analysis for the overall control system and a performance analysis in terms of contouring and tracking accuracy at steady state. A computer simulation was used to demonstrate the validity of the proposed methodology. The performance variation was investigated under different operating conditions and controller gains, and a design range was elicited that met the given performance specifications. The results provide basic guidelines in systematic and comprehensive controller designs for multi-axis CNC systems. A cross-coupling control system was also implemented on a PC-based three-axis CNC testbed, and the experimental results confirmed the usefulness of the proposed control system in terms of contouring accuracy.

모멘텀 바이어스 인공위성의 2축 자세제어 시스템 설계 (Two Axis Attitude Control System Design of Momentum Biased Satellite)

  • 이승우;서현호
    • 한국항공우주학회지
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    • 제34권4호
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    • pp.40-46
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    • 2006
  • 위성기술의 비약적 발달에 따라서 설계 및 제작에 소용되는 비용은 저렴하지만 신뢰도가 높은 인공위성 자세제어 시스템 개발이 요구되고 있다. 본 연구는 이러한 요구를 만족시키기 위해 반작용휠에 의한 모멘텀 바이어스 벡터가 임의의 방향(태양 방향)을 지향하고 안정화되는 위성시스템을 제시하였다. 위성 시스템에서 고장 가능성이 가장 적은 자기장 센서, 저정밀 태양센서 및 자기토커를 센서와 구동기로 사용하였으며, 고전적 선형 제어방법에 의해 2축 제어하는 제어시스템 설계방법을 제시하였다. 제어기는 PD 형태의 간단한 제어기가 사용되었고, 선형화된 위성시스템에 대한 PD 제어기 설계방법이 적절한 가정과 함께 제시되었다. 제시된 제어기 설계방법에 의해 설계된 폐루프 시스템의 장기 안정성 검증을 위해서 비선형 시뮬레이션 방법을 사용하였다.

4축 힘/토크 센서의 구조 설계 (Design of Structure of Four-Axis Force/Torque Sensor with Parallel Step Plate Beams)

  • 이경준;김갑순
    • 제어로봇시스템학회논문지
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    • 제20권11호
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    • pp.1147-1152
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    • 2014
  • This paper describes the design of a four-axis force/torque sensor with PSPBs (Parallel Step Plate Beams). The sensor is composed of eight PSPBs, a force/torque transmitting block, and fixing blocks. It is designed by using the FEM(Finite Element Method), and fabricated by using strain gages. The characteristic tests of the sensor are carried out, and the interference error, repeatability error, and non-linearity error are less than 2.21%, 0.03% and 0.03%. Furthermore, the structure of the four-axis force/torque sensor with PSPBs has a larger rated capacity than that of the four-axis force/torque sensor with PPBs under the same overall sensor size and the same rated output. It is thought that the developed four-axis force/torque sensor with PSPBs can be used for measuring the forces and torques in an intelligent robot, automation devices, etc.

스카라 로봇 암의 최적화 설계 및 시뮬레이션 (Optimal Design and Simulation of SCARA Robot Arm)

  • 이종신
    • 제어로봇시스템학회논문지
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    • 제15권6호
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    • pp.612-618
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    • 2009
  • This study is concerned about the optimal design of the arm 1 and arm 2 in the SCARA robot. The mass and inertia moment of the arm I and arm 2 in a SCARA robot is greatly affected on the performance such as a cycle time, and torques loaded on $1^{st}$ axis and $2^{nd}$ axis. To reduce the mass and inertia moment, this study carried out optimal design by FEM analysis using parametric variables, which is a width, a height of the rib and a thickness of arm in the arm. The rib is adapted instead of reducing the thickness in the arm. And the simulation by computer was conducted on two given paths in X direction and Y direction. After optimal design, the result showed that maximum torque of $1^{st}$ axis and $2^{nd}$ axis reduced to maximum 9.5% on a given path.

KAUSatSIM을 이용한 한누리 2호 자세제어 알고리즘 검증 (Verification of KAUSAT-2 Satellite Attitude Control Algorithm Using KAUSatSIM Simulator)

  • 나희승;이병훈;장영근
    • 한국항공우주학회지
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    • 제36권5호
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    • pp.514-523
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    • 2008
  • 본 논문에서는 한누리 2호의 자세제어 알고리즘 검증을 위해 개발한 KAUSatSIM에 대해서 논의한다. KAUSatSIM은 6개의 에어베어링을 사용하여 무마찰 환경을 모사한 1축 회전 테이블과 한누리 2호에서 사용된 각종 센서 및 모멘텀 휠로 구성되어 있다. 이 시뮬레이터는 한누리 2호의 자세제어 알고리즘에 대한 검증과 새로운 제어 알고리즘 개발, 그리고 그 성능 검증에 사용될 수 있다. 개발된 1축 회전 시뮬레이터를 이용하여 한누리 2호 개발에 이용된 자세제어 알고리즘 검증을 위하여 모멘텀 휠을 이용한 시험을 수행하였다. 비례-미분제어기를 사용한 모멘텀 휠 제어기를 설계하여 좋은 실험 결과를 얻었다. 그리고 더 나아가 추력기 시스템을 추가하여 소형위성에 적용 가능한 새로운 알고리즘 개발 및 검증이 가능하도록 하였다.

외란 관측기를 이용한 중앙 분산형 다두 자수기의 동기제어 (Synchronous Control of Center Distributed Multi-Head Embroidery Machine Using Disturbance Observer)

  • 정승현;최득성;박정일
    • 한국정밀공학회지
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    • 제31권11호
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    • pp.1015-1021
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    • 2014
  • This paper proposes the center distributed embroidery machine structure with 1,500 RPM, 52 heads for productivity and large sized embroidery goods. The synchronous velocity controller is adopted for control of the 2-axis distributed embroidery machine and the DOB(Disturbance Observer) is also adopted for minimizing disturbances caused by needle cams. For driving experiments of 2-axis center distributed driving structure, two conventional 26 heads 1,500RPM embroidery machines are used. It was shown that the center distributed driving structure with 2-axis synchronous control can be one way for implementing a large embroidery machine.