• 제목/요약/키워드: Unmodeled dynamics

검색결과 80건 처리시간 0.042초

시간 지연 추정을 이용한 강인 Backstepping 제어 (Robust Backstepping Control Using Time Delay Estimation)

  • 김성태;장평훈;강상훈
    • 대한기계학회논문집A
    • /
    • 제28권12호
    • /
    • pp.1833-1844
    • /
    • 2004
  • A controller is proposed for the robust backstepping control of a class of nonlinear multiple-input multiple-output (MIMO) systems which can be converted to a strict feedback form. The proposed robust backstepping control scheme follows a systematic procedure for the design of control laws and uses time delay estimation (TDE) to estimate the uncertainties such as parameter variations, unknown disturbances, and unmodeled dynamics, etc. The proposed controller can be also applied to nonlinear MIMO systems with unmatched uncertainties. Stability analysis of the closed-loop system which contains the plant and the proposed controller is also studied and hereby a sufficient stability condition for the closed-loop system is proposed. The simulation results show that the control scheme works well with uncertainties and the proposed stability condition is valid. The controller is experimentally verified on a single-link flexible arm to show the effectiveness of the proposed scheme in the complicated systems with uncertainties.

Finite-Time Nonlinear Disturbance Observer Based Discretized Integral Sliding Mode Control for PMSM Drives

  • Zheng, Changming;Zhang, Jiasheng
    • Journal of Power Electronics
    • /
    • 제18권4호
    • /
    • pp.1075-1085
    • /
    • 2018
  • To deal with the operation performance degradation of permanent magnet synchronous machine (PMSM) drives with uncertainties and unmodeled dynamics, this paper presents a finite-time nonlinear disturbance observer (FTNDO) based discretized integral sliding mode (DISM) composite control scheme. Based on the reaching-law approach, a DISM speed controller featuring a superior dynamic quality and global robustness against disturbances is constructed. This controller can avoid the reaching phase and overlarge control action. In addition, a sliding mode differentiator based FTNDO is devised and extended to the discrete-time domain for disturbance estimation. The attractive features of the FTNDO are that it can provide a finite-time converging estimation and alleviate the chattering effect in conventional sliding mode observers, while retaining robustness to parameter variations. By feeding the estimate forward to the pre-stage DISM controller, both disturbances and chattering can be significantly suppressed. Moreover, considering the estimation error of a FTNDO caused by discrete sampling, a stability analysis of the composite controller is discussed. Experimental results validate the superiority of the presented scheme.

규정된 추종오차 구속제어와 유한시간 슬라이딩 모드 제어를 이용한 로봇시스템의 미지의 외란에 대한 강인제어 (Robust Control for Unknown Disturbance of Robotic System Using Prescribed Tracking Error Constraint Control and Finite-Time SMC)

  • 류현제;신동석;한성익
    • 제어로봇시스템학회논문지
    • /
    • 제22권5호
    • /
    • pp.320-325
    • /
    • 2016
  • This paper presents a robust finite-time sliding mode control (SMC) scheme for unknown disturbance and unmodeled nonlinear friction and dynamics in the robotic manipulator. A finite-time SMC (FSMC) surface and finite-time sliding mode controller are constructed to obtain faster error convergence than the conventional infinite-time based SMC. By adding prescribed constraint control term to a finite-time SMC to compensate for unknown disturbance and uncertainties, a robust control scheme can be designed as well as faster convergence control. In addition, simpler controller structure is built by using feed-forwarding upper bound coefficients of each manipulator dynamic parameters instead of model-based control or adaptive observer to estimate unknown manipulator parameters. Simulation and experimental evaluations highlight the efficacy of the proposed control scheme for an articulated robotic manipulator.

내재된 입력성형기: 사다리꼴 프로파일과 S-커브 프로파일의 차이 (Embedded Input Shaper: Difference between Trapezoidal Profile and S-curve Profile)

  • 하창완;이동욱;윤병호;류근호;김경수
    • 제어로봇시스템학회논문지
    • /
    • 제20권11호
    • /
    • pp.1125-1130
    • /
    • 2014
  • In this paper, we discuss the relation between the motion profile and pre-filter. As previously reported in various literatures [1-3], a tuned motion profile can effectively reduce residual vibration by placing inherent zeros of the motion profile at the vibratory pole of systems similar to the role of the input shaping technique. From the results, we factorize the motion profile into a basis function and an input shaper. In contrast to the previously reported impulse-sequence-based input shapers, the input shaper extracted from the motion profile has unique characteristics. Thanks to the characteristics of the input shaper extracted from the motion profile, it has advantages to reduce the vibrations caused by not only the modeled vibratory mode but also unmodeled dynamics which exist in higher frequency ranges.

자기베어링으로 지지된 연삭 스핀들의 런아웃 제어 -LMS Feedforward 제어를 이용한 실험적 해석- (Runout Control of Mgenetically Suspended Grinding Spindle - Experimental Analysis of Adaptive LMS Feedforward Control Method -)

  • 노승국;경진호;박종권;최언돈
    • 한국정밀공학회:학술대회논문집
    • /
    • 한국정밀공학회 2000년도 추계학술대회 논문집
    • /
    • pp.997-1001
    • /
    • 2000
  • In this paper, the case studies of reducing rotational errors is theoretically done for a grinding spindle with an active magnetic bearing system. The rotational errors acting on the magnetic bearing spindle are due to mass unbalance of rotor, runout, grinding excitation and unmodeled nonlinear dynamics of electromagnets. For the most case, the electrical runout of sensor target is big even in well finished surface, this runout can cause a rotation error amplified by feedback control system. The adaptiveed forward method based on LMS algorithm is discussed to compensate this kind of runout effects, and investigated its effectiveness by numerical simulation and experimental analysis. The electrical runout form the rear sensor target of grind spindle is about 70$\mu\textrm{m}$ with harmonic frequencies. The rotor orbit size in rear bearing is reduced about to 5$\mu\textrm{m}$ due to 1X and 2X rejection by feedforward control.

  • PDF

슬라이딩 모드 제어를 위한 인자 튜닝 알고리듬 (Parameter Tuning Algorithm for Sliding Mode Control)

  • 류세희;박장현
    • 한국정밀공학회:학술대회논문집
    • /
    • 한국정밀공학회 2003년도 춘계학술대회 논문집
    • /
    • pp.438-442
    • /
    • 2003
  • For an efficient sliding mode control system stability and chattering avoidance should be guaranteed. A continuation method using boundary layer is well known as one solution for this. However since not only model uncertainties and disturbances but also control task itself is variable. it is practically impossible to set controller parameters - control discontinuity, control bandwidth, boundary layer thickness - in advance. In this paper first an adaptation law of control discontinuity is introduced to assure system stability and then fuzzy logic based tuning algorithm of design parameters is applied based on monitored performance indices of tracking error, control chattering, and model precision. In the end maximum control bandwidth not exciting unmodeled dynamics and minimum control discontinuity, boundary layer thickness making system stable and free of chattering are found respectively. This eliminates control chattering and enhances control accuracy as much as possible under given control situation. In order to demonstrate the validity of the proposed algorithm safe headway maintenance control for autonomous transportation system is simulated. The control results show that the proposed algorithm guarantees system stability all the time and tunes control parameters consistently and in consequence implements an efficient control in terms of both accuracy and actuator chattering.

  • PDF

비선형 스위칭 평면을 가지는 적응가변구조 제어기 설계 (A study on the Adaptive Variable Structure Controller with Nonlinear Switching Surfaces)

  • 박수식;이대식
    • 대한전기학회:학술대회논문집
    • /
    • 대한전기학회 1996년도 추계학술대회 논문집 학회본부
    • /
    • pp.52-54
    • /
    • 1996
  • A number of algorithm using the VSS(Variable Structure System) for uncertain dynamic system are developed. But, in these algorithms, the assumption that the uncertainties are bounded and their bounds are available to the designer is involved. And bounds on the uncertainties are an important clue to guarantee the stability of the closed loop system. However, sometimes bounds on the uncertainties may not be easily obtained because of the complexity of the structure of the uncertainties. Therefore, a methodology by which the boundary values on the uncertainties can be easily obtained is required. The VSS proposed in this proposal employ the new adaptive VSS scheme for uncertain dynamic system being estimated on line. The resulting control law is simple and easy to apply to on line computer control. It can also suppress chattering and maintain good tracking precision even if unmodeled dynamics are considered. And, a new method using nonlinear switching surface is introduced so that the speed response is improved and the good transient response can be obtained. Simulation results are presented and show the advantage of the proposed adaptive VSS with nonlinear switching surfaces.

  • PDF

컨테이너크레인 시스템의 슬라이딩모드제어 (Sliding-Mode Control of Container Cranes)

  • 이숙재;박한;홍금식
    • 한국항해항만학회지
    • /
    • 제29권8호
    • /
    • pp.747-753
    • /
    • 2005
  • 본 논문은 컨테이너크레인의 흔들림제어의 한 방법으로, 이송증인 컨테이너가 임의의 이송궤적을 따라서 움직이도록 하고, 또한 트롤리 및 호이스트의 위치제어를 동시에 수행하는 가변구조제어에 관한 연구이다. 자동화터미널의 야석장에서 A지점에서 B지점으로 컨테이너를 옮기고자 할 때, 쌓여 있는 주위의 다른 컨테이너들을 피하면서 이송시키거나, 혹은 양하역 작업을 장애물이 존재하는 환경에서 수행할 때 주변의 장애물과 충돌하지 않도록 이송궤적을 만들어야 함은 필수적이다. 기존치 연구들이 무조건 흔들림이 작게끔 하는 것에 초점을 맞추었던 것에 반하여 본 논문에서는 비롯 흔들림이 발생하더라도 주어진 궤적을 추종하여 이송되게끔 하는 것에 그 특징이 있다. 트롤리 및 호이스트의 위치 및 속도오차 뿐 아니라 흔들림 각변위 및 각속도오차가 슬라이딩 평면으로 정의되며, 등속구간과 도착구간에서의 제어기가 각각 별도로 설계된다. 리아프노프 방법을 이용하여 안정성을 해석하였으며 파일럿 크레인을 이용한 실험결과를 제시한다.

급변하는 환경에서의 인간의 의사결정과 상황파악 (Sensemaking and Human Judgment Under Dynamic Environment)

  • 성연호;박의현;이화기
    • 대한인간공학회지
    • /
    • 제25권3호
    • /
    • pp.49-60
    • /
    • 2006
  • Technological encroachment provides human operators with flood of information that must be analyzed to understand the environment and make judgments that lead to strategic actions. Further, the environment is not static and therefore uncertain, changing its aspect dynamically. Complexity accompanied with its dynamics imposes substantial difficulty to human operators' task. Criticality of having situational understanding becomes more important than ever. Situationalunderstanding requires the human operators possessing tacit knowledge in order for them to make the sense out of the situation while interacting with information from many heterogeneous sources, the notion of sensemaking. Sensemaking refers to the process of developing mental framework to assemble pieces of information representing different aspects of the environment that can be used to develop one's own actionable knowledge to implement their judgments in the uncertain environment. Therefore, judgment process and performance is a key component of sensemaking process. Among many judgment and decision making models, the lens model with its extension can be utilized to partially describe the judgmental aspect of sensemaking. One of the lens model parameters, unmodeled knowledge, can be a corresponding quantitative measure for the tacit knowledge that plays an important role in sensemaking. In this paper, a comprehensive literature for sensemaking is provided to formally define the notion of sensemaking in the military domain. Also, it is proposed that there is a crucial link between the sensemaking and human judgment process and performance from the lens model perspective. Potential implications for experimental framework are also proposed.

이중 주파수 GPS 데이터를 이용한 저궤도 위성의 정밀궤도결정 (Precise Orbit Determination of LEO Satellite Using Dual-Frequency GPS Data)

  • 황유라;이병선;김재훈;윤재철
    • Journal of Astronomy and Space Sciences
    • /
    • 제26권2호
    • /
    • pp.229-236
    • /
    • 2009
  • 다목적실용위성-5호는 2010년 발사를 목표로 고도 550km의 저궤도에 위치하게 될 것이다. 다목적실용위성-5호의 임무인 고정밀 SAR(Synthetic Aperture Radar) 영상을 처리하기 위해서는 정확한 위성의 위치(20cm) 와 속도(0.03cm/s)가 결정되어야 한다. 이러한 요구 조건은 한국 전자통신연구원에서 개발한 ETRI GNSS Precise Orbit Determination(EGPOD) 소프트웨어로 검증하였다. 0.1Hz 수신 주기의 SAC-C 위성 반송파위상 데이터로 정밀궤도결정을 수행하였다. 이중 주파수 GPS 데이터를 사용하여 수신 선호의 전리층 오차를 대부분 제거하고 이중 차분된 데이터를 생성함으로써 GPS 위성과 수신기의 공통된 시계 오차를 없앴다. 동역학 모델 접근 방법을 이용하였고, Batch Least Square Estimator(BLSE) 필터로 각 데이터 아크(arc) 에 해당하는 위성의 위치와 속도, 대기저항 계수, 태양풍 계수를 추정하였다. 또한 정밀한 동역학 모델을 위하여 모델 되지 않은 부정확한 가속도 항을 보충하는 경험 가속도를 추가하였다. 경험 가속도는 위성의 공전 주기(revolution) 당 한번씩 시선방향(radial), 진행방향(along-track), 수직방향(cross-track)으로 추정하고, 수직방향의 상수 항에 대해서는 해당 데이터 아크에 관하여 부가적으로 추정하였다. 정밀궤도결정 결과 검증을 위하여 EGPOD 소프트웨어에서 얻어진 결과와 JPL에서 제공하는 정밀궤도력(Precise Orbit Ephemeris)을 비교하였다.