• Title/Summary/Keyword: HILS 시스템

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The Engagement HILS Technology Research in the Laboratory for Simulated Warfare between Electronic Warfare Equipment and High-speed Maneuvering Weapon System (실험실에서 전자전 장비와 고속 기동 무기체계 간 실 교전 모의용 조우 HILS 기술 연구)

  • Shin, Dongcho;Choe, Wonseok;Kim, Soyeon;Lee, Chiho
    • Journal of the Korea Society for Simulation
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    • v.28 no.2
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    • pp.49-57
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    • 2019
  • In this paper, we describe the implementation methods and algorithms for the various technologies and devices required for the construction of the engagement HILS(Hardware In the Loop Simulation) in the limited space to simulate the high-speed maneuvering encounter situation of the weapon system in 3-dimensional real world space. Through this research, we have been able to suggest ways to analyze the major design elements of future electronic warfare equipment through experiments simulating actual engagements between various high-speed maneuvering weapons systems and electronic warfare devices in the future battlefield. It was confirmed that the M&S technology could be used to eliminate technical risks, reduce development cost, and shorten development time in the future real system development. The results of this study can be a great assist not only for the field of electronic warfare system research and development, but also for the research & implementation on HILS of various engaging class weapons systems.

The control strategy for Steer-by-Wire test system

  • Jang, Seok-Hwan;Chae, Ho-Chol;Oh, Se-Wook;Han, Chang-Soo;Park, Tong-Jin;Yun, Seok-Chan
    • 제어로봇시스템학회:학술대회논문집
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    • 2002.10a
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    • pp.75.4-75
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    • 2002
  • $\textbullet$ Introduction $\textbullet$ Steer by wire(SBW) $\textbullet$ HILS System $\textbullet$ SBW Control Algorithm $\textbullet$ SBW-HILS $\textbullet$ Simulation $\textbullet$ Conclusion

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Hardware-in-the-loop simulation of RPV autopilot using strapdown AHRS (스트랩다운 AHRS를 이용한 무인항공기(RPV) 자동조종장치의 실시간 실물 모의시험)

  • 홍성경;김태연;탁민제
    • 제어로봇시스템학회:학술대회논문집
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    • 1992.10a
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    • pp.135-140
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    • 1992
  • This paper presents the configuration, HILS procedure and performance simulation results of the RPV autopilot including a strapdown AHRS. Real time hardware-in-the-loop simulation was performed by using a 3 axis flight motion simulator alonged assumed flight trajectory of the RPV. Being compared with the result of the 6 DOF simulation, the HILS results showed that the performance of the autopilot was satisfactory.

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The Study on LCS Embedded Design of Traffic Signal Evaluation System HILS (교통신호 평가시스템 HILS에서의 LCS 임베디드 설계 연구)

  • Kim, Bong seob;Lee, Jeong jun;Koo, Seung Hoe
    • The Journal of The Korea Institute of Intelligent Transport Systems
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    • v.18 no.6
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    • pp.1-10
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    • 2019
  • Traffic Signal Evaluation HILS is a system designed to evaluate a traffic signal system, and has a function of driving that simulates a real environment using a simulator that simulates a real traffic signal environment and an LCS that simulates a traffic signal controller. This study simulates the function of the traffic signal controller and is designed for design the LCS which is connected to the center system and the traffic simulator (VISSIM). The design of the LCS program uses a portable python language, and the code is designed in two versions running on Windows in the PC environment and unning on embedded environment, with a slight modification of the code. In this study, we analyzed the limitations of using LCS on Windows in PC environment and confirmed the ease of simulation Linux in embedded environment at large capacity.

Development of Operation Scenarios by HILS for the Energy Storage System Operated with Renewable Energy Source (HILS를 이용한 신재생 에너지원이 포함된 에너지 저장시스템의 운영 시나리오 개발)

  • Shin, Dong-Cheol;Jeon, Jee-Hwan;Park, Sung-Jin;Lee, Dong-Myung
    • The Transactions of The Korean Institute of Electrical Engineers
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    • v.67 no.2
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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.

Modelling of Fixed Wing UAV and Flight Control Computer Based Autopilot System Development for Integrated Simulation HILS Environment (고정익 UAV 모델링 및 비행조종컴퓨터 기반 오토파일럿 통합 시뮬레이션 HILS 환경 구축)

  • Kim, Lamsu;Lee, Dongwoo;Lee, Hohyeong;Hong, Suwoon;Bang, Hyochoong
    • Journal of the Korean Society for Aeronautical & Space Sciences
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    • v.50 no.12
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    • pp.857-866
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    • 2022
  • Fixed-wing UAVs have long endurance and range capabilities compared to other aerial platforms. These advantages led fixed-wing UAVs to become a popular platform for reconnaissance missions in the military. In this research, we modeled fixed-wing UAVs, including the landing gear model and developed a guidance and control system for flight control computers to construct a HILS environment. We also developed an autopilot system that includes automated take-off, cruise, and landing control for UAVs. We also retrived the Aerodynamic coefficients an UAV using Datcom and AVL software and used them for 6 degrees of freedom modeling. The Flight control computer calculates guidance commands using the Carrot chasing guidance law after distinguishing the condition of the UAV based on 16 pre-defined flight modes and calculates control inputs using Nonlinear Dynamic Inversion (NDI) control scheme. We used RTNngine to integrate the Simulink model and flight control computer for HILS environment formulation.

Development of Real Time Vehicle Dynamics Models for Intelligent Vehicle HILS (지능형 차량 HILS를 위한 실시간 차량 동역학 모델 개발)

  • Lee, Chang-Ho;Kim, Sung-Soo;Jeong, Wan-Hee;Lee, Sun-Ho
    • Transactions of the Korean Society of Automotive Engineers
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    • v.14 no.4
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    • pp.199-206
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    • 2006
  • Real time vehicle dynamics models have been developed with the subsystem synthesis method for intelligent vehicle HILS system. Three different models for solving subsystem equations are compared in order to find out the best suitable model for HILS applications. The first model is based on the generalized coordinate partitioning technique, and the second one is on the approximate function approach, and the last one is on the constraint stabilization method. To investigate the theoretical efficiency of three proposed methods, arithmetic operators used in the formulations of three models are counted. Bump run simulations with half-sine bump have also carried out with three different models to measure the actual CPU time to validate theoretical investigation.

A Verification of a Sensorless BLDC Motor Drive System to Control 4-axis Fins for a Guided Artillery Munition by HILS (유도형 탄약의 4축 조종날개 제어용 Sensorless BLDC 전동기 구동시스템 개발 및 HILS에 의한 검증)

  • Lee, Tae-Hyung;Kim, Sang-Hoon;Cho, Chang-Yeon;Pak, Chang-Ho;Kim, Jae-Ho
    • The Transactions of the Korean Institute of Power Electronics
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    • v.20 no.6
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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.

Implementation and Test of 3-level NPC VSC-HVDC System using Hardware-in-the-Loop Simulation (Hardware-in-the-Loop Simulation을 이용한 3-레벨 NPC 전압형 HVDC 시스템 구현 및 테스트)

  • Yoo, Hyeong-Jun;Kim, Nam-Dae;Kim, Hak-Man
    • The Transactions of The Korean Institute of Electrical Engineers
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    • v.63 no.3
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    • pp.343-348
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    • 2014
  • Recently, applications of VSC-HVDC systems to power systems are growing because of their control ability of reactive power. Meanwhile, the hardware-in-the-loop simulation (HILS) based on the real-time digital simulator has been applying to develop and test imbedded controllers and systems in the power industry to decrease costs and to save time. In this paper, a 3-level neutral point clamped (NPC) VSC-HVDC system is modeled and the embedded controllers of the NPC VSC-HVDC system are designed. The designed controllers are implemented by TMS320F28335. The TMS320F28335-based controllers of the NPC VSC-HVDC system are tested using the HILS.