• Title/Summary/Keyword: Integrated Control System

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The Development of Cloud Computing-Based Integrated EHS Management System for the Construction Companies (클라우드 컴퓨팅 기반 건설사용 EHS 통합관리시스템 개발)

  • Seo, Kwang-Kyu
    • Proceedings of the KAIS Fall Conference
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    • 2010.11b
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    • pp.859-861
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    • 2010
  • The construction companies are facing potential EHS(Environment, Health & Safety) of major accidents to cause casualties or a financial loss and increasing social responsibility. So, they have to voluntarily accomplish the EHS management system rather than passively with regard to EHS regulation. In this study, the integrated EHS management system is developed based on cloud computing, and construction companies are to materialize self-regulation EHS process of construction workplace and to standardize the total EHS business process using the developed system. The proposed system also provides risk analysis, education/control and continuous improvement for EHS tasks and users can easily access the system on the web at a low price through cloud computing service. Eventually, the integrated system contributes to the managerial improvement by minimizing economic and physical loss caused by construction accidents.

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Design and Construction of Integrated Signalling System for Next-generation High-Speed Train (한국형 고속전철용 통합 신호시스템의 설계 및 구축)

  • 황종규;이종우;조용기;류호중
    • Proceedings of the KSR Conference
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    • 2002.05a
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    • pp.467-472
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    • 2002
  • The railway signal ing system consists of several vital computerized equipments. Now the project for development of signal ing system for the next-general ion high-speed train is progressed according to the consortium. The developing signal ing system by this project, kTCS(Korean Train Control System), is composed of kTCS-CTC, kTCS-IXL, kTCS-ATC and etc. The KTCS signaling has to be operated as a integrated system by interface between each signaling. To achieve these, communicat ion protocols between each signal ing have to be designed and message codes are defined. In this paper the configuration of integrated kTCS system and designed communication protocol is presented.

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A Hybrid Fire Fighting Control Intelligent System using Rules and Cases in Integrated Platform Management System (통합플랫폼관리체제에서 규칙 및 사례기반의 하이브리드 화재진압통제 지능시스템)

  • 현우석;김용기
    • Journal of Intelligence and Information Systems
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    • v.6 no.2
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    • pp.15-27
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    • 2000
  • The paper proposes a hybrid fire fighting control intelligent system(H-FFIS) using rules and cases to detect fire in Integrated Platform Management System. By far most conventional systems have been based on rule-based system in which expert knowledges are expressed with production rules. It is hard to express the knowledges to detect fire with production rules only. The knowledges of fire detection are often based on previously encountered situations of fires. For improvement of system capability renewing and adding of rules is needed in an already build-up system and such adding and renewing procedures could hinder users from fluent utilization of the system. We design and implement H-FFIS. Compared with rule-based FFIS(Fire Fighting control Intelligent System), H-FFIS extended with case-based reasoning shows that the system proposed here can lead to an improvement in fire detection rate.

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Development of a UAV Flight Control System Using a Low Cost GPS/IMU (저가형 GPS/IMU를 이용한 UAV 비행 제어 시스템 개발)

  • Koo, Won-Mo;Chun, Se-Bum;Won, Dae-Hee;Kang, Tae-Sam;Lee, Young-Jae;Sung, Sang-Kyung
    • Journal of Institute of Control, Robotics and Systems
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    • v.14 no.5
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    • pp.502-510
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    • 2008
  • UAVs(Unmanned Aerial Vehicles) have many applications in military and commercial areas. The flight control system of UAVs is more important than manned aircraft's because the mission of UAVs must be operated without a human pilot. But very heavy and expensive navigation system makes it difficult to develop UAV flight control system. In this research, GPS/IMU integrated navigation filter was developed for light weight/low cost flight control system of small UAVs. With this navigation filter, full flight control system which has real time operating capability has been developed. The performance of the flight control system is basically checked by HILSIM (Hardware In the Loop SIMulation). Finally, the flight control system is verified by showing performance test result under real flight environment.

Profile-based TRN/INS Integration Algorithm Considering Terrain Roughness (지형 험준도를 고려한 프로파일 기반 지형참조항법과 관성항법의 결합 알고리즘)

  • Yoo, Young Min;Lee, Sun Min;Kwon, Jay Hyun;Yu, Myeong Jong;Park, Chan Gook
    • Journal of Institute of Control, Robotics and Systems
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    • v.19 no.2
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    • pp.131-139
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    • 2013
  • In recent years alternative navigation system such as a DBRN (Data-Base Referenced Navigation) system using geophysical information is getting attention in the military navigation systems in advanced countries. Specifically TRN (Terrain Referenced Navigation) algorithm research is important because TRN system is a practical DBRN application in South Korea at present time. This paper presents an integrated navigation algorithm that combines a linear profile-based TRN and INS (Inertial Navigation System). We propose a correlation analysis method between TRN performance and terrain roughness index. Then we propose a conditional position update scheme that utilizes the position output of the conventional linear profile type TRN depending on the terrain roughness index. Performance of the proposed algorithm is verified through Monte Carlo computer simulations using the actual terrain database. The results show that the TRN/INS integrated algorithm, even when the initial INS error is present, overcomes the shortcomings of linear profile-based TRN and improves navigation performance.

An Integrated On-Line Diagnostic System for the NORS Process of Maiden Reactor Project: The Design Concept and Lessons Learned

  • Kim, Inn-Seock
    • Nuclear Engineering and Technology
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    • v.32 no.3
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    • pp.261-273
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    • 2000
  • During an extensive review made as part of the Integrated Diagnosis System project of the Maiden Reactor Project, MOAS (Maryland Operator Advisory System) was identified as one of the most thorough systems developed thus far. MOAS is an integrated on-line diagnosis system that encompasses diverse functional aspects that are required for an effective process disturbance management: (1) intelligent process monitoring and alarming, (2) on-line sensor data validation and sensor failure diagnosis, (3) on-line hardware (besides sensors) failure diagnosis, and (4) real-time corrective measure synthesis. The MOAS methodology was used at the Maiden Man-Machine Laboratory HAMMLAB of the OECD Maiden Reactor Project. The performance of MOAS, developed in G2 real-time expert system shell for the high-pressure preheaters of the NORS process in the HAMMLAB, was tested against a variety of transient scenarios, including failures of the control valves and sensors, and tube leakage of the preheaters. These tests showed that MOAS successfully carried out its intended functions, i.e., quickly recognizing an occurring disturbance, correctly diagnosing its cause, and presenting advice on its control to the operator. The lessons learned and insights gained during the implementation and performance tests also are discussed.

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Development of Unmanned Aerial Vehicle System Integration Laboratory(UAV SIL) for the Integrated Verification (무인항공기 체계의 통합검증을 위한 무인항공기 체계통합실험실(UAV SIL) 개발)

  • Jae Ick Shim;Hee Chae Woo;Sang Jin Kim;Sang Jun Jung
    • Journal of the Korea Institute of Military Science and Technology
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    • v.27 no.1
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    • pp.70-79
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    • 2024
  • This paper describes the results of the development of the the unmanned aerial vehicle system integration laboratory(UAV SIL) for the integrated verification. This UAV SIL is designed to test the robustness of the UAV system including the operational logics and the flight control system behaviors under many abnormal and emergency conditions such as data-link losses, airborne subsystem failures, engine shut down conditions, and ground control station faults. This paper presents how to build the UAV SIL and how to verify the in-development UAV system through the UAV SIL.

Reliable $H_{\infty}$ Controller Design for a Class of Uncertain Linear Systems with Actuator Failures

  • Dai, Shi-Lu;Zhao, Jun
    • International Journal of Control, Automation, and Systems
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    • v.6 no.6
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    • pp.954-959
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    • 2008
  • This paper is concerned with the reliable $H_{\infty}$ controller design problem for uncertain linear systems against actuator failures. In the design, the $H_{\infty}$ performance of the closed-loop system is optimized during normal operation(without failures) while the system satisfies a prescribed $H_{\infty}$ performance level in the case of actuator failures. Single and parameter-dependent Lyapunov function approaches are applied in designing suboptimal reliable $H_{\infty}$ controllers. Simulation studies are presented to demonstrate the effectiveness of the proposed design procedures.

Development of Conversational Interface Platform Based on MS Robotics Studio for Integrated Service Robots (통합 서비스 로봇을 위한 MS 로보틱스 스튜디오 기반 대화 인터페이스 플랫폼 구축)

  • Lim, Sung-Soo;Cho, Sung-Bae
    • The Journal of Korea Robotics Society
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    • v.4 no.1
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    • pp.49-55
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    • 2009
  • The development of IT technology makes the functions and services of robots be integrated, and thus the robots become more intelligent and useful. As sophisticated usage of robots has evolved, direct communication by human language is necessary to increase the efficiency of their usage. In this paper, we propose a conversational interface platform for integrated service robots using MS Robotics Studio. The proposed platform consists of three types of components: a conversation manager to control the flows of the integrated service robots, a user interface to interact with users, and multiple service robots to perform actions or services. For a test-bed of the proposed platform, we build a schedule manager system and confirm the usability through SUS subject test by comparing the schedule manager system with MS Outlook.

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Development of Low-Cost Automatic Flight Control System for an Unmanned Target Drone (무인표적기용 저가형 자동비행시스템 개발)

  • Lee, Jang-Ho;Ryu, Hyeok;Kim, Jae-Eun;Ahn, Iee-Ki
    • Journal of Advanced Navigation Technology
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    • v.8 no.1
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    • pp.19-26
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    • 2004
  • This paper deals with the automatic flight control system for an unmanned target drone which is operated by an army as an anti-air gun shooting training. By automation of unmanned target drone that is manually operated by external pilot, pilot can reduce workload and an army can reduce the budget. Most UAVs which are developed until today use high-cost sensors as AHRS and IMU to measure the attitude, but those are contradictory for the reduction of budget. This paper says the development of low-cost automatic flight control system which makes possible of automatic flight with low-cost sensors. We have developed the integrated automatic flight control system by integrating electricity module, switching module, monitoring module and RC receiver as an one module. We also prove the performance of automatic flight control system by flight test.

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