• 제목/요약/키워드: Control Requirements

검색결과 2,393건 처리시간 0.026초

직무기반 접근제어 모델 설계 (A Design of Role-Based Access Control Model)

  • 이호;정진욱
    • 한국컴퓨터정보학회논문지
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    • 제6권1호
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    • pp.60-66
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    • 2001
  • 본 논문에서는 접근제어 요구 사항의 복잡한 문제를 해결하기 위한 직무기반 접근제어 모델을 설계하였다. 본 논문에서 설계한 접근제어 모델은 직무기반 접근제어를 이용하여 권한을 효과적으로 통제하고, 신분 및 규칙기반 접근제어를 이용하여 정보의 비밀성, 무결성 및 가용성의 보장과 불법적인 유통을 방지할 수 있다. 설계된 접근제어 모델은 직무, 보안등급, 무결성 등급 및 소유권 등의 다단계 보안 정책을 기반으로 하여 자원에 대한 불법적인 접근을 방어 할 수 있다

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Servo Drives State of the Art in Industrial Applications - A Survey

  • Kennel R.;Kobs G.;Weber R.
    • 전력전자학회:학술대회논문집
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    • 전력전자학회 2001년도 Proceedings ICPE 01 2001 International Conference on Power Electronics
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    • pp.321-325
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    • 2001
  • Servo drives with microcomputer control provide the possibility of using modem and sophisticated control algorithms. As an additional feature it is possible to implement parallel and/or redundant software and hardware structures to realise safe motion or similar security functions. Unfortunately microcomputer control also has some impact on the behaviour of servo drives. Control algorithm, cycle time, sensors and interface have to be perfectly synchronised. Special control schemes are necessary on the line side (power supply) to meet the actual requirements concerning EMC. This contribution presents experiences and results obtained from a modem digital drive system pointing out the influences of low and high accuracy position sensors and the interdependencies mentioned above.

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Spacecraft Formation Reconfiguration using Impulsive Control Input

  • Bae, Jonghee;Kim, Youdan
    • International Journal of Aeronautical and Space Sciences
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    • 제14권2호
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    • pp.183-192
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    • 2013
  • This paper presents formation reconfiguration using impulsive control input for spacecraft formation flying. Spacecraft in a formation should change the formation size and/or geometry according to the mission requirements and space environment. To modify the formation radius and geometry with respect to the leader spacecraft, the follower spacecraft generates additional control inputs; the two impulsive control inputs are general control type of the spacecraft system. For the impulsive control input, Lambert's problem is modified to construct the transfer orbit in relative motion, given two position vectors at the initial and final time. Moreover, the numerical simulation results show the transfer trajectories to resize the formation radius in the radial/along-track plane formation and in the along-track/cross-track plane formation. In addition, the maneuver characteristics are described by comparing the differential orbital elements between the reference orbit and transfer orbit in the radial/along-track plane formation and along-track/cross-track plane formation.

다수의 혼잡 노드와 멀티개스트 연결을 가지는 비동기 전송망의 ABR 서비스에 대한 혼잡 제어 (Congestion Control for the ABR Service of ATM networks with Multiple Congested Nodes and Multicast Connections)

  • 노지명;임종태
    • 제어로봇시스템학회논문지
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    • 제6권8호
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    • pp.629-637
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    • 2000
  • Unbalance between user requirements and insufficient network resources makes a congestion. In the future since the communication networks will have very heavy traffic congestion will be more serious. The ATM networks was recommended to support the B-ISDN service for the future multimedia communication. In thie sense of congestion avoidance and recovery the ABR service category in ATM networks allows the feedback flow control mechanism to dynamically allocate the idle bandwidth of the network to users fairly and to control the network congestion rapidly In this paper we introduce a congestion control scheme using systematical approach to confirm robust stability with respect to unknown round trip delay for the network which has both unicast and multicast connections.

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Impact control of redundant manipulators using null-space dynamucs

  • Chung, W.J.;Choi, S.L.;kim, I.H.;Chung, G.J.
    • 제어로봇시스템학회:학술대회논문집
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    • 제어로봇시스템학회 1994년도 Proceedings of the Korea Automatic Control Conference, 9th (KACC) ; Taejeon, Korea; 17-20 Oct. 1994
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    • pp.89-94
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    • 1994
  • This paper presents an impact control algorithm for reducing the potentially damaging effects by interation of redundant manipulators with their environments. In the. proposed control algorithm, the redundancy is resolved at the torque level by locally minimizing joint torque, subject to tire operational space dynamic formulation which maps tire joint torque set into the operational forces. For a given pre-impact velocity of the manipulator, the proposed approach is on generating joint space trajectories throughout the motion near the contact which instantaneously minimize the impulsive force which is a scalar function of manipulator's configurations. This is done by using the null space dynamics which does not affect the motion of an end-effector. The comparative evaluation of the proposed algorithm with a local torque optimization algorithm without reducing impact is performed by computer simulation. The simulation results illustrate the effectiveness of the algorithm in reducing both the effects of impact and large torque requirements.

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전동 부스터의 슬라이딩 모드 제어 (Sliding Mode Control of Electric Booster System)

  • 양이진;최규웅;허건수
    • 제어로봇시스템학회논문지
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    • 제18권6호
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    • pp.519-525
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    • 2012
  • Electric brake booster systems replace conventional pneumatic brake boosters with electric motors and rotary-todisplacement mechanisms including ECU (Electronic Control Unit). Electric booster brake systems require precise target pressure tracking and control robustness because vehicle brake systems operate properly given the large range of loading and temperature, actuator saturation, load-dependent friction. Also for the implement of imbedded control system, the controller should be selected considering the limited memory size and the cycle time problem of real brake ECU. In this study, based on these requirements, a sliding mode controller has been chosen and applied considering both model uncertainty and external disturbance. A mathematical model for the electric booster is derived and simulated. The developed sliding mode controller considering chattering problem has been compared with a conventional cascade PID controller. The effectiveness of the controller is demonstrated in some braking cases.

원자력 발전소 제어계통을 위한 네트워크의 해석과 사례 연구 (Analysis of a network for control systems in nuclear power plants and a case study)

  • 이성우;임한석
    • 제어로봇시스템학회논문지
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    • 제5권6호
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    • pp.734-743
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    • 1999
  • In this paper, a real-time communication method using a PICNET-NP(Plant instrumentation and Control Network for Nuclear Power plant) is proposed with an analysis of the control network requirements of DCS(Distributed Control System) in nuclear power plants. The method satisfies deadline in case of worst data traffics by considering aperiodic and periodic real-time data and others. In addition, the method was used to analyze the data characteristics of the DCS in existing nuclear power plant. The result shows that use of this method meets the response time requirement(100ms).

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Nonlinear Observer-based Control of Synchronous Machine Drive System

  • Sundrica, Marijo;Erceg, Igor;Maljkovic, Zlatko
    • Journal of Electrical Engineering and Technology
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    • 제10권3호
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    • pp.1035-1047
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    • 2015
  • Starting from a new dynamic system description novel synchronous machine deterministic observers are proposed. Reduced and full order adaptive observer variations are presented. Based on the feedback linearization control law and the use of deterministic observer a novel control system is built. It meets the requirements of high performance tracking system. Adaptivity to stator and rotor resistance and the torque sensorless application is included. The comparison of the proposed novel control with conventional linear and nonlinear control systems is discussed. The given simulational study includes complete drive system integration.

Design and Control of a Marine Satellite Antenna

  • Won Mooncheol;Kim Sung-Soo
    • Journal of Mechanical Science and Technology
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    • 제19권spc1호
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    • pp.473-480
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    • 2005
  • A three axes marine satellite antenna has been developed. As a design step, a CAD model for the antenna has been created according to the design requirements. Kinematic analyses are carried out to insure design specification and to check collision detection of the CAD model. Marine satellite antennas experience base motions, and a relevant control system should control the three antenna axis to point to the satellites accurately. A sensor fusion algorithm and a PIDA (Proportional, Integral, Derivative, Acceleration) control algorithm are designed and implemented to control the yaw, level, and cross-level angle of a small size satellite marine antenna. Antenna stabilization control experiments are performed using a test simulator which gives the antenna base motions. Experimental results show small pointing errors, which is less than 0.2 degree for the level, cross-level, and yaw axis.

Profibus-DP에서의 원격 피드백 제어 시스템 구축 (Implementation of Remote Feedback Control System via Profibus-DP Network)

  • 이경창;강송;이석
    • 한국정밀공학회지
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    • 제18권5호
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    • pp.120-129
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    • 2001
  • As many sensors and actuators are used in many automated systems, various industrial networks are adopted for real-time distributed control. In order to take advantages of the networking, however, the network implementation should be carefully designed to satisfy real-time requirements considering network delays. This paper presents the implementation of a remote feedback control system via Profibus-DP net work for real-time distributed control More specifically, the effect of the network delay on the control performance evaluated on Profibus-DP testbed. Also, the traditional PID gain tuning methods are used to demonstrate the feasibility of the remote feedback control.

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