• 항공우주기술
• /
• 제3권1호
• /
• pp.9-15
• /
• 2004

본 논문에서는 무인비행선 비행제어시스템의 HILS(Hardware-In-the-Loop-Simulation) 시스템 개발 결과를 소개한다. HILS 시스템은 비행선 제어를 위해 설계된 비행제어컴퓨터의 지상시험을 위해 개발되었다. HILS 시스템을 구성하기 위해 각각 별도의 컴퓨터에서 작동하는 통신장비 모사 시스템, 탑재장치 모사 시스템, 비행선 운동 모사 시스템, 그리고 운동 가시화 시스템을 개발하였고, 이와 함께 3축 운동 시험대와 관성항법장치(Inertial Navigation Unit)도 포함하였다. 개발된 HILS 시스템을 이용한 단계적인 시험을 통해 비행 제어컴퓨터의 기능과 성능을 검증하였다.

• International Journal of Automotive Technology
• /
• 제7권6호
• /
• pp.687-695
• /
• 2006

This paper presents a network-based traction control system(TCS), where several electric control units(ECUs) are connected by a controller area network(CAN) communication system. The control system consists of four ECUs: the electric throttle controller, the transmission controller, the engine controller and the traction controller. In order to validate the traction control algorithm of the network-based TCS and evaluate its performance, a Hardware-In-the-Loop Simulation(HILS) environment was developed. Herein we propose a new concept of the HILS environment called the network-based HILS(Net-HILS) for the development and validation of network-based control systems which include smart sensors or actuators. In this study, we report that we have designed a network-based TCS, validated its algorithm and evaluated its performance using Net-HILS.

• 대한전기학회:학술대회논문집
• /
• 대한전기학회 1999년도 하계학술대회 논문집 B
• /
• pp.566-568
• /
• 1999

HILS is widely used in the test and evaluation of complex control system. This paper describes the structure of HILS and the control loop performance monitoring of HILS system Distal path delay and FMS(Flight Motion Simulator) dynamics were estimated and output of the estimated model were compared with real FMS output. The monitoring system can be used for analyzing the result of HILS.

• 한국군사과학기술학회지
• /
• 제13권5호
• /
• pp.785-792
• /
• 2010

This paper on the Research of Naval Electronic Warfare System HILS(Hardware In the Loop System) describes the EW engagement HILS construction method for evaluation of the operational concept analysis on active RF Decoy in staying in the air and the deceit ability to anti-ship missile seeker. We obtain the EW M&S technology of EW engagement HILS and EW efficiency analysis from this project. This Naval Electronic Warfare System HILS technology will support Active Decoy Development Project and any other HILS of EW weapon in KOREA ARMY/NAVY/AIR FORCE.

• 제어로봇시스템학회논문지
• /
• 제21권9호
• /
• pp.881-887
• /
• 2015

The hardware-in-the-loop simulation (HILS) of a railway vehicle is crucial for overcoming the limitation of field tests of a railway vehicle. A brake HILS system for a railway vehicle was previously not able to test the performance of a speed-sensing system of a railway vehicle, since wheelset speeds were generated only by computer simulations. In this paper, we present a novel wheelset speed implementation of a brake HILS system for a railway vehicle. Four wheelset speeds of a brake HILS system for a car of a railway vehicle are implemented using four small-sized servomotors, whereas the speed sensors and pole wheels used in the brake HILS system are the actual ones of the railway vehicle. According to the simulated speeds of four wheelsets in the dynamic equations of motion, four servomotors generate wheel speeds in real time, and then the measured wheelset speeds are fed back to the computer simulation model. Moreover, in this paper, we improve the performance of wheelset speed measurement via the T method instead of the M method presently used in the field. The performances of wheelset speed implementation and speed-sensor operation are demonstrated by experimental works using a HILS system.

• 대한기계학회논문집A
• /
• 제24권12호
• /
• pp.2883-2890
• /
• 2000

In this study, a Hardware-In-The-Loop-Simulation(HILS) system for developing a Electric-Power-Steering(EPS) system is designed. To test a EPS by HILS system, a mathematical vehicle model with a steering system model has been constructed. This mathematical model has been constructed. This mathematical model has been downloaded to the Digital-Signal-Processor(DSP) board. To realize the lateral force acting on the front wheel in a real car. the steering wheel angle sensor and vehicle velocity have been used for input signal. The force sensor has been used for a feedback signal. The full vehicle states could by simulated by the HILS system. Consequently, the HILS system could by used to analyze control-parameters of a EPS that contributes to the maneuverability and stability of a vehicle. At the same time, the HILS system can evaluate the whole performance of the vehicle-steering system. Also the HILS system could do test could not be executed in real vehicle. The HILs system will useful for developing the control logic for the EPS system.

• 한국자동차공학회논문집
• /
• 제14권5호
• /
• pp.47-57
• /
• 2006

This paper presents a network-based traction control system(TCS), where several electric control units (ECUs) are connected by a controller area network(CAN) communication system. The control system consists of four ECUs: the electricthrottle controller, the transmission controller, the engine controller and the traction controller. In order to validate the traction control algorithm of the network-based TCS and evaluate its performance, a Hardware-In-the-Loop Simulation(HILS) environment was developed. Herein we propose a new concept of the HILS environment called the network-based HILS(Net-HILS) for the development and validation of network-based control systems which include smart sensors or actuators. In this study, we report that we have designed a network-based TCS, validated its algorithm and evaluated its performance using Net-HILS.

• 한국항공우주학회지
• /
• 제37권7호
• /
• pp.701-708
• /
• 2009

개발된 비행제어컴퓨터(DFLCC: Developed Flight Control Computer)의 비행제어법칙은 고등훈련기급 항공기의 시제 최종 형상의 비행제어소프트웨어(OFP: Operation Flight Program)를 기반으로 개발되었다. 비행제어법칙은 상용 개발 툴을 이용하여 GUI(Graphic User Interface) 환경에서 설계되며, C 코드로 변환되어 OFP 에 반영된다. 그리고 OFP는 정형화된 검증절차를 통하여 검증되는데, 검증과정을 거치기 전에 비실시간 환경에서 C코드로 변환된 비행제어법칙과 기반이 되는 비행제어법칙의 상사성(similarity)을 검증하고, 구성된 HILS(Hardware In-the-Loop Simulator) 환경의 신뢰성(reliability)을 사전에 검증하는 절차가 필요하다. 비행제어법칙의 상사성은 비실시간 환경에서 고등훈련기급 항공기의 시제 최종 버전의 비행제어법칙과 개발된 비행제어법칙의 응답특성을 상호 비교하여 검증된다. 또한, 구성된 HILS 환경의 신뢰성은 비실시간 시뮬레이션 툴을 기반으로 HILS 결과와 항공기 응답특성을 비교하여 검증된다. 본 논문에서는 항공기 응답을 직접 비교함으로써 개발된 비행제어법칙의 상사성과 HILS 환경의 신뢰성을 검증하였다.

• 항공우주기술
• /
• 제3권1호
• /
• pp.170-178
• /
• 2004

본 논문은 KSR-III 개발경험을 토대로 모션테이블을 이용한 로켓 6자유도 실시간모의시험(HILS) 방안에 대해 다루고 있다. 모션테이블 HILS 시험을 통해, 3축 모션테이블의 동특성 지연에 따른 제어루프의 안정성을 판단하고 종합 HILS 시험을 위한 기초 자료를 제공하게 된다. 모션테이블 HILS 초기화 시험을 통해, 관성항법장치 초기정렬을 위한 초기자세 각 유지 알고리듬 시험, 발사시작 신호 모사를 통한 시각동기화 시험, 외부기록계를 이용한 실시간 조정시험 등을 수행하게 되고, 개루프 HILS 시험을 통해 정상 상태 비행 상황 및 슬로싱, 벤딩, TWD, 바람, 추력비정렬오차 등의 영향이 존재하는 비행 상황에 대한 모션테이블 운용 시험을 수행하게 되며, 최종적으로 모션테이블 자세각을 궤환루프의 입력으로 궤환시킨 폐루프 HILS를 통해 제어루프의 안정성 시험을 완료하게 된다.

• 한국자동차공학회논문집
• /
• 제7권6호
• /
• pp.165-173
• /
• 1999

HILS system consists of hardwares which are engine and dynamometer and softwares which is vehicle model without the engine. It is well-known that because of engines's nonlinearity it is difficult to describe an engine exactly and not to lose it reality coincidently. But HILS system is the high technology that can compensate this weakness by using a real engine instead of model. The various experiments regarding the ACC which are not normally available for real vehicle tests have been performed by the HILS system. From the results , the HILS system is expected to decrease the experimental accident rate and save costs and time. Compared with simulation, HILS experimental results show similarities and expected to increase road capacity.