• 항공우주기술
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• 제8권1호
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• pp.172-178
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• 2009

최근에 개발된 소형제트기는 조종사의 피로경감과 더불어 비행안전성 제고를 위하여 자동비행시스템이 필수적인 요소로 인식되고 있다. 또한, 소형항공기의 항공전자시스템은 집중화된 다중프로세서(centralized multi-processor)와 다중연산 계산구조(multi-process computing architectures)로서 B-777의 Integrated Modular Avionics와 유사한 시스템을 장착하는 추세이다. 이러한 소형항공기 시스템 변화는 고전적 비행방식인 조종사 중심의 비행방식에서 자동비행제어시스템(AFCS) 중심의 비행방식으로의 변화를 야기하였으며 자동 비행제어시스템의 비중은 보다 더 증가하고 있다. 이에 본 논문에서는 상용 소형항공기용 자동비행장치(Autopilot)에 대한 HILS를 구성하여 성능을 검증하였다. 또한, 현재 개발하고 있는 FBW용 FCC(Flight Control Computer)에 탑재될 자동비행 알고리듬에 대한 성능을 PILS를 통하여 확인하였고, 상용 Autopilot에 대한 HILS 결과와 같은 조건에서 비교하여 그 성능을 검증하였다.

• 전기학회논문지
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• 제67권2호
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• pp.224-232
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• 2018

According to government policy, renewable energy facility such as solar power generation is being implemented for newly constructed buildings. In recent years, the introduction of Energy Storage System (ESS) served as an emergency power for replacing an existing diesel generator has been increasing. Furthermore, in order to expand the efficacy of the ESS operation, operation in combination with renewable energy sources such as solar and wind power generation is increasing. Hence, development of the ESS operation algorithms for emergency mode as well as the peak power cut mode, which is the essential feature of ESS, are necessary. The operational scenarios of ESS need to consider load power requirement and the amount of the power generation by renewable energy sources. For the verification of the developed scenarios, tests under the actual situation are demanded, but there is a difficulty in simulating the emergency operation situation such as system failure in the actual site. Therefore, this paper proposes simulation models for the HILS(Hardware In the Loop Simulation) and operation modes developed through HILS for the ESS operated with renewable energy source under peak power reduction and emergency modes. The paper shows that the ESS operation scenarios developed through HILS work properly at the actual site, and it verifies the effectiveness of the control logic developed by the HILS.

• 한국소음진동공학회:학술대회논문집
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• 한국소음진동공학회 2009년도 추계학술대회 논문집
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• pp.351-356
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• 2009

This paper presents vibration control performance of active engine mount system installed with the magneto-rheological (MR) mount and the piezostack mount. The performance is evaluated via hardware-in-the-loop-simulation(HILS) method. As a first step, six degrees-of freedom dynamic model of an in-line four-cylinder engine which has three points mounting system is derived by considering the dynamic behaviors of MR mount and piezostack mount. As a second step, sliding mode controller(SMC) is synthesized to actively control the imposed vibration In order to demonstrate the effectiveness of the proposed active engine mount, vibration control performances are evaluated under various engine operating speeds (wide frequency range) using HILS method and presented in time and frequency domain.

• 한국정밀공학회:학술대회논문집
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• 한국정밀공학회 2003년도 춘계학술대회 논문집
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• pp.1139-1143
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• 2003

HILS(Hardware-In-the-Loop Simulation) is a scheme that incorporates hardware components of primary concern in the numerical simulation environment. Due to its advantages over actual vehicle test and pure simulation, HILS is being widely accepted in automotive industries as test benches for vehicle control units. Developed in this study is a HILS system for EHB(Electro-Hydraulic Brake) systems that include a high pressure generator and a valve control system that independently modulates the brake pressures at four wheels. An EHB control logic was tested in the HILS system. Test results under various driving conditions are presented and compared with the VDC logic.

• 한국소음진동공학회논문집
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• 제20권2호
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• pp.122-128
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• 2010

This paper presents vibration control performance of active engine mount system installed with the magneto-rheological(MR) mount and the piezostack mount. The performance is evaluated via hardware-in-the-loop-simulation(HILS) method. As a first step, six degrees-of freedom dynamic model of an in-line four-cylinder engine which has three point mounting system is derived by considering the dynamic behaviors of MR mount and piezostack mount. As a second step, sliding mode controller(SMC) is synthesized to actively control the imposed vibration. In order to demonstrate the effectiveness of the proposed active engine mount, vibration control performances are evaluated under various engine operating speeds(wide frequency range) using HILS method and presented in time and frequency domain.

• 한국자동차공학회논문집
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• 제7권8호
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• pp.172-179
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• 1999

This paper presents a simple but effective DYC algorithm which enhances vehicle lateral stability by using an anti=lock brake system (ABS). In the proposed algorithm, only the front outer wheel is controlled during cornering maneuver instead of controlling all four wheels because the wheel has the largest role in DYC and it is easy and simple to control the only one wheel. An ABS Hardware - In -The -Loop Simulation ( HILS) system that may be used to realistically test real vehicle dynamic behavior in a lab is used for evaluating the proposed DYC algorithm in severe situations where a vehicle is destabilized without DYC . The HILS results show that the proposed DYC algorithm has the potential of maintaining vehicle stability in some dangerous situations.

• 제어로봇시스템학회:학술대회논문집
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• 제어로봇시스템학회 2003년도 ICCAS
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• pp.1714-1719
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• 2003

Antilock Brake System (ABS) is indispensable safety equipment for vehicles today. In order to develop new ABS ECU suitable for pneumatic brake system of a bus, a Hardware In-the-Loop Simulation (HILS) System was developed. In this HILS, the pneumatic brake system of a bus and antilock brake component were used as hardware. For the computer simulation, the 14-Degree of Freedom (DOF) bus dynamic model was constructed using the Matlab/Simulink software package. This model was compiled and downloaded in the simulation board, where the Power PC processor was used for real-time simulation. Additional commercial package, the ControlDesk was used to monitor the dynamic simulation results and physical signal values. This paper will focus on the procedure and results of evaluating the ECU in the HILS simulation. Two representative cases, wet basalt road and $split-{\mu}$ road, were used to simulate real road conditions. At each simulated road, the vehicle was driven and stopped under the help of the developed ECU. In each simulation, the dynamical behavior of the vehicle was monitored. After enough tests in the laboratory using HILS, the parameter-tuned ECU was equipped in a real bus, which was driven and stopped in the real test field in Korea. And finally, the experiment results of ABS equipped vehicle's dynamic behavior both in HILS test and in test fields were compared.

• 한국항행학회논문지
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• 제27권5호
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• pp.574-579
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• 2023

레이다 비행시험은 다양한 조건의 표적, 클러터, 재밍을 모의하는데 많은 제약 사항이 있다. 따라서, 본 연구에서는 운용 시나리오에 따라 운용 모의 기능을 수행하는 레이다 비행 모의 장치를 개발하였다. 개발된 레이다 비행모의 장치는 레이다 빔 운용 모의, 레이다 동작 제어, 모의 신호 발생, 비행자세모의를 통해 레이다의 다양한 임무 환경을 모의한다. 레이다 비행모의 장치는 레이다 임무 환경(클러터, 재밍 등)이 포함된 모의 표적(단일, 다중) 신호를 생성하고 변조하여 RF를 통해 레이다로 송신한다. 개발된 레이다 비행모의장치와 AESA 레이다를 연동하여, 다양한 비행 시나리오를 기반으로 하여 모의 표적을 탐지하고 탐지 결과 확인을 통해 레이다 성능을 검증하였다.

• 한국컴퓨터정보학회논문지
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• 제18권12호
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• pp.55-64
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• 2013

본 논문에서는 전투기에 탑재되어 지상표적을 추적하고 레이저를 조사하여 레이저유도 폭탄을 유도하는 등의 기능을 수행하는 타겟팅파드의 성능분석 및 검증을 위한 HILS(Hardware In-the-Loop Simulation) 시스템 구축에 대하여설명한다. 타겟팅파드의실시간 성능분석을위해서는 주간카메라와IR카메라의 모의영상생성기술, 서보제어기술 및 레이저 전달 특성 분석기술이 필요하다. 실시간 모의 영상생성과 레이저 전달 특성 분석에는 검증된 상용 소프트웨어 개발 키트(SDK)인 OKTAL-SE를 활용하였고, 서보구동은 실제 유사과제에서 적용된 서보구동의 메커니즘을 적용하여 정확도를 높였다. 또한, 실제 전투기 인터페이스와 동일한 조건의 성능분석을 위하여 1553B, ARINK818 등의 인터페이스를 실제 구현하여 적용하였다. 본 논문에서 구축한 HILS 시스템을 적용하면 현재 운용되는 전투기 장착 탑재전자체의 성능분석과 검증은 물론 실제 장비 개발 중 각 모듈의 성능이 시스템 전체 성능에 미치는 영향도 분석가능하다. 향후 다양한 비행체의 비행역학을 적용하여 광범위한 분야에 활용가능 함으로 개발요구사항 도출 및 개발 위험을 줄이는 데 큰 기여를 할 수 있을 것으로 예상된다.

• 전력전자학회논문지
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• 제20권6호
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• pp.580-586
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• 2015

A brushless DC (BLDC) motor control system for four-axis driving fins to control the flight attitude of a guided artillery munition is developed in this study. This system adopts a simple sensorless control scheme without a Hall sensor. A 12-step driving sensorless BLDC motor scheme is used to improve the output torque. This system has many restrictive problems that hinder the verification of a real system. For example, this has cost and environmental limitations. Therefore, this study develops HILS to verify a four-axis driving fin control system and verifies the position control system hardware by HILS operation.