• 제목/요약/키워드: HILS(Hardware-in-the Loop Simulation)

검색결과 194건 처리시간 0.026초

다상 BLDC 모터 드라이브 시스템의 개방 고장 시 효율 향상이 고려된 토크 리플 저감 대책 (Torque Ripple Reduction Method With Enhanced Efficiency of Multi-phase BLDC Motor Drive Systems Under Open Fault Conditions)

  • 김태윤;서용석;박현철
    • 전력전자학회논문지
    • /
    • 제27권1호
    • /
    • pp.33-39
    • /
    • 2022
  • A multi-phase brushless direct current (BLDC) motor is widely used in large-capacity electric propulsion systems such as submarines and electric ships. In particular, in the field of military submarines, the polyphaser motor must suppress torque ripple in various failure situations to reduce noise and ensure stable operation for a long time. In this paper, we propose a polyphaser current control method that can improve efficiency and reduce torque ripple by minimizing the increase in stator winding loss at maximum output torque by controlling the phase angle and amplitude of the steady-state current during open circuit failure of the stator winding. The proposed control method controls the magnitude and phase angle of the healthy phase current, excluding the faulty phase, to compensate for the torque ripple that occurs in the case of a phase open failure of the motor. The magnitude and phase angle of the controlled steady-state current are calculated for each phase so that copper loss increase is minimized. The proposed control method was verified using hardware-in-the-loop simulation (HILS) of a 12-phase BLDC motor. HILS verification confirmed that the increase in the loss of the stator winding and the magnitude of the torque ripple decreased compared with the open phase fault of the motor.

스마트 무인기의 지상시험을 통한 비행제어 성능분석 (Assessment of Flight Control Performance based on the Ground Test Results of Smart UAV)

  • 강영신;박범진;유창선;김유신;구삼옥
    • 항공우주기술
    • /
    • 제9권1호
    • /
    • pp.1-8
    • /
    • 2010
  • 스마트무인기의 비행시험에 앞서 비행제어시스템을 포함한 전체 무인기 체계의 건전성을 검증하기위한 지상통합시험을 수행하였다. 지상통합시험은 비행체 인터페이스 시험, 비행체 HILS시험, 지상파워시험, 4자유도 치구시험, 안전줄 호버시험 순서로 진행되었으며, 각각의 시험을 통해 전체 무인기 시스템의 안전성을 입증하였다. 본 논문에서는 국내 최초로 개발된 틸트로터인 스마트무인기의 지상시험 절차와 각 시험에서 획득한 데이터 분석결과를 제시하였다. 지상시험 결과 비행제어시스템의 안전성이 충분히 입증되었으며, 비행시험이 수행가능하다고 판단되었다.

Experiments of Force Control Algorithms for Compliant Robot Motion

  • Kim, Dong-Hee;Park, Jong-Hyeon;Song, Ji-Hyuk;Hur, Jong-Sung
    • 제어로봇시스템학회:학술대회논문집
    • /
    • 제어로봇시스템학회 2004년도 ICCAS
    • /
    • pp.1786-1790
    • /
    • 2004
  • The main objective of this paper is to analyze the performance of various force control algorithms in improving and adjusting the compliance of industrial robots in contact with their environment. Some of fundamental force control algorithms such as sensorless control, impedance control and hybrid position/force control are theoretically analyzed and simulated for various situations of an environment, and then a series of experiments using them were performed. In this paper, a control scheme to use position control in implementing the impedance control was investigated in order to nullify the effect of joint friction. The new reference trajectory is generated using contact force feedback and original desired trajectory. And an inner position control loop is designed to provide accurate position tracking for the new reference trajectory and good disturbance rejection. Experiments to insert a peg in a hole (so-called the peg-in-a-hole task) were performed with HILS (hardware-in-theloop simulation) system based on the results of the analyses and simulations on the characteristics of each control algorithm. The experiments showed that various force control methods improved the performance of robots in close contact with the environment by adjusting their compliance with respect to an arbitrary set of coordinates.

  • PDF

원적외선 호밍 유도탄 시험을 위한 가상 해상 환경의 구현 (Implementation of Virtual Maritime Environment for LWIR Homing Missile Test)

  • 박혜령
    • 한국군사과학기술학회지
    • /
    • 제19권2호
    • /
    • pp.185-194
    • /
    • 2016
  • It is essential for generating the synthetic image to test and evaluate a guided missile system in the hardware-in-the-loop simulation. In order to make the evaluation results to be more reliable, the extent of fidelity and rendering performance of the synthetic image cannot be left ignored. There are numerous challenges to simulate the LWIR sensor signature of sea surface depending on the incident angle, especially in the maritime environment. In this paper, we investigate the key factors in determining the apparent temperature of sea surface and propose the approximate formula consisting of optical characteristics of sea surface and sky radiance. We find that the greater the incident angle increases, the larger the reflectivity of sea surface, and the greater the water vapor concentration in atmosphere increases, the larger the amount of sky radiance. On the basis of this information, we generate the virtual maritime environment in LWIR region using the SE-WORKBENCH, physically based rendering software. The margin of error is under seven percentage points.

인덕터 내부저항을 고려한 LCL 필터의 능동댐핑 특성 (Active Damping Characteristics on Virtual Series Resistances of LCL Filter for Three-phase Grid-connected Inverter)

  • 김용중;김효성
    • 전력전자학회논문지
    • /
    • 제21권1호
    • /
    • pp.88-93
    • /
    • 2016
  • LCL filters are widely used in high-order harmonics attenuation of output currents in grid-connected inverters. However, output currents of grid-connected inverters with LCL filters can become unstable because of the resonance of the filters. Given that the characteristics of output currents in inverters mostly depend on filter performance, the exact analysis of filters by considering parasitic components is necessary for both harmonics attenuation and current control. LCL filters have three or four parasitic components: the series and/or parallel resistance of the filter capacitor and the series resistance of the two filter inductors. Most studies on LCL filters have focused on the parasitic components of the filter capacitor. Although several studies have addressed the parasitic components of the filter inductor at the inverter side, no study has yet investigated the concurrent effects of series resistance in both filter inductors in detail. This paper analyzes LCL filters by considering series resistance in both filter inductors; it proposes an active damping method based on the virtual series resistance of LCL filters. The performance of the proposed active damping is then verified through both simulation and experiment using Hardware-in-the-Loop Simulator(HILS).

추정된 타이어 힘을 이용한 능동 조향 제어 (Active steering Control Based on The Estimated Tire Forces)

  • 서찬원;김준영;홍대건;허건수
    • 대한기계학회논문집A
    • /
    • 제24권9호
    • /
    • pp.2228-2234
    • /
    • 2000
  • Steering of the vehicles on a slippery highway is a difficult task for most passenger car drivers. The steering vehicles on slippery roads tend to slide outward with less lateral forces than on nor mal roads. When the drivers notice that their vehicles on a slippery highway start to depart from the cornering lane, most of them make a sudden steering and/or braking, which in turn may induce spin-out and instability on their vehicles. In this paper, an active steering control method is proposed such that the vehicles in slippery roads are steered as if they are driven on the normal roads. In the proposed method, the estimated lateral forces acting on the steering tires are compared with the reference values and the difference is compensated by the active steering method. A fuzzy logic controller is designed for this purpose and evaluated on a steering Hardware-In-the-Loop Simulation (HILS) system. Steering performance results on the slippery curved and sinus roads demonstrate the effectiveness of the proposed controller. This method can be realized with the steer-by-wire concept and is promising as an active safety technology.

온도 변화에 따른 ER 엔진마운트의 제어 특성 (Control Characteristics of ER engine mount considering Temperature Variation)

  • 송현정;최승복
    • 한국소음진동공학회:학술대회논문집
    • /
    • 한국소음진동공학회 2005년도 춘계학술대회논문집
    • /
    • pp.180-183
    • /
    • 2005
  • The engine mount of vehicle systems is role of support engine mass and isolate noise and vibration from engine disturbance forces. One of attractive candidates to achieve this goai is to utilize a semi-active ER engine mount. By applying this, we can effectively control damping force and hence the noise and vibration by just controlling the intensity of electric field. However, control performance of the engine mount may be very sensitive to temperature variation during engine operation. In this work, we Investigate dynamic performances of ER engine mount with respect to the temperature variation. In order to undertake this, a flow-mode type of ER engine mount is designed and manufactured. Displacement transmissibility is experimentally and numerically evaluated as a function of the electric field. The ER engine mount is then incorporated with full-vehicle model in order to investigate vibration control performance. After formulating the governing equation of motion, a semi-active controller is designed. The controller is implemented through a hardware-in-the-loop simulation (HILS), and control responses such as acceleration level at various engine speeds are evaluated in the frequency and time domains.

  • PDF

Fault Detection System Design and HILS Evaluation for the Smart UAV FCS

  • Nam, Yoon-Su;Jang, Hu-Yeong;Hong, Sung-Kyung;Park, Sung-Su
    • International Journal of Control, Automation, and Systems
    • /
    • 제5권1호
    • /
    • pp.104-109
    • /
    • 2007
  • This paper is about a redundancy management system design for the Smart UAV(unmanned aerial vehicle) which utilizes the tilt..rotor mechanism. In order to meet the safety requirement on the PLOC(probability of loss of control) of $1.7{\times}10^{-5}$ per flight hour for FCS (flight control system) failures, a digital FCS is mechanized with a dual redundant structure. A fault detection system which is composed of a CCM(cross channel monitor) and analytic redundancy using the Kalman filtering is designed, and its effectiveness is evaluated through experiments. A threshold level and persistence count for managing redundant sensors are designed based on the statistical analysis of the FCS sensors. To increase the survivability of the UAV after the loss of critical sensors in the SAS(stability augmentation system) and to provide reference information for a tie-breaking condition at which an ILM(in-line monitor) cannot distinguish the faulty channel between two operating ones, the Kalman filter approach is investigated.

온도변화에 강인한 EPB 시스템의 모델기반 고장검출 방법 (Robust Model Based Fault Detection of EPB System for Varying Temperature)

  • 문병준;박종국
    • 한국자동차공학회논문집
    • /
    • 제17권5호
    • /
    • pp.26-30
    • /
    • 2009
  • In this paper, a robust model based fault detection for varying temperature is proposed, To develop a robust force estimation model, it needs temperature information because the force sensor's output is affected by a temperature variation. If an EPB system does not include a temperature sensor, the model has a much larger error than an EPB system with a built-in temperature sensor. Therefore, the temperature is estimated by using Ohm's law. The force model is applied with a motor current, battery voltage, operation mode, and the estimated temperature to detect a force sensor's abnormal signal fault. The residual is calculated by comparing the value of the measured force and the estimated force. Fault information is collected by using the output of the evaluated residual with the adaptive thresholds. A proposed robust model based fault detection for varying temperature was verified by HILS (Hardware in the Loop Simulation).

능동 표적신호 합성 (MOving Spread Target signal simulation)

  • 성낙진;김재수;이상영;김강
    • 한국음향학회지
    • /
    • 제13권2호
    • /
    • pp.30-37
    • /
    • 1994
  • 최근 표적의 고속화와 저표적강도화 추세에 따라 표적 탐지의 정확성이 요구되고 있다. 본 연구는 이에 부합하여 표적 운동 해석, 표적 분류, 소나 성능 예측 모델의 개발에 필수적인 표적 산란 잔향 신호의 주파수 및 시간별 특성의 파악과 그러한 특성을 포함한 표적 신호 시뮬레이션에 목적을 두고 있다. 표적 신호 시뮬레이션에는 음향 변환자 배열의 음원 준위와 빔패턴으로 구성되는 음원모델, 전달 손실 예측부인 환경모델, 복합 표적에 의한 신호의 신장 및 표적 강도와 음원과 표적의 상대운동을 표현하는 도플러 현상이 고려된 표적모델, 수신기의 감도 및 빔패턴과 각 채널의 시간이 고려된 수신 모델 등 주요한 4부분의 모델이 필요하다. 개발된 MOST(MOving Spread Target) 신호합성기는 환경모델을 제외한 3가지 모델로 구성 되어 있으며, 음원과 표적의 운동에 의한 신호 특성 시뮬레이션 등의 기능을 갖추고 있어, 소나 운용 체계 개발의 한 단계인 HILS(Hardware In the Loop Simulation)와 표적 상태 추정을 위한 신호 특성 분석 및 앞에서 언급한 각종 모델에서 신호 발생 장치로 이용될 수 있다.

  • PDF