• 제목/요약/키워드: Maneuvering Controller

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DGPS를 이용한 자동 운항 제어기 설계 및 개발 (Design and Development of Automatic Maneuvering Controller Using DGPS)

  • 김기영;이명일;허석;곽문규
    • 제어로봇시스템학회논문지
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    • 제12권9호
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    • pp.850-855
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    • 2006
  • This is concerned with the development and design of automatic maneuvering system using Differential Global Positioning System(DGPS). To achievement of autonomous maneuvering controller for giant ship, first, we investigated automatic maneuvering controller using DGPS in motor car. The sensors are configured with DGPS and digital compass. We calculated velocity and steering angle of motor car based on sensor signal. To design the controller, we derived the bicycle model and developed critically damped controller. The critically damped controller can be tracing previously appointed position in the fastest time. We are used a laptop computer to realize and the control algorithm is programmed by visual basic software. The obtained experimental results from developed system show unmanned motor car is good tracing planed positions. Hence, the system is looking forward to use the autonomous maneuvering control fur giant ship.

선박 자동 운항 제어기의 설계 (Design of Automatic Ship Maneuvering Control System)

  • 곽문규;서상현
    • 한국해양환경ㆍ에너지학회지
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    • 제2권1호
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    • pp.90-101
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    • 1999
  • 본 논문은 선박자동 항로 추적제어기와 자동접이안 제어기를 포함하는 선박자동운항시스템 설계와 관련이 있다. 자동항로 추적제어기의 설계를 위해서는 최적제어기가 사용되었는데 선형화된 선박조종식이 사용되었다. 수치예는 자동항로 추적제어기가 선장이 미리정한 way point를 추적할 수 있음을 보여주고 있다. 자동접이안 제어기의 설계를 위해서는 비중앙화 방식의 제어기가 사용되었다. 자동접이안 제어기는 자동 항로 추적 제어기에 전진속도에 대한 퍼지 로직 제어기가 추가 되어 실현되었다 수치예는 자동접이안 제어기가 성공적으로 사용되었음을 보여준다.

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Design and Application of an Adaptive Neural Network to Dynamic Positioning Control of Ship

  • Nguyen, Phung-Hung;Jung, Yun-Chul
    • 한국항해항만학회:학술대회논문집
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    • 한국항해항만학회 2006년도 International Symposium on GPS/GNSS Vol.1
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    • pp.285-290
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    • 2006
  • This paper presents an adaptive neural network based controller and its application to Dynamic Positioning (DP) control system of ship. The proposed neural network based controller is developed for station-keeping and low-speed maneuvering control of ship. At first, the DP system configuration is described. And then, to validate the proposed DP system, computer simulations of station-keeping and low-speed maneuvering performance of a multi-purpose supply ship are presented under the influence of measurement noise, external disturbances such as sea current, wave, and wind. The simulations have shown the feasibility of the DP system in various maneuvering situations.

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수중운동체의 조종제어기 설계연구 (A Study on the Design of a Maneuvering Controller for Submersible Vehicles)

  • 양승윤;이만형
    • 대한기계학회논문집A
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    • 제20권3호
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    • pp.850-860
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    • 1996
  • This paper considers a sliding mode controller for a depth and course control of a class of submersible Vehicles. Since the vehicle used here shows complex dynamic characteristics sensitive to speed variation and buoyancy, robustness in control of vertical and horizontal plane motions of the vehicle is achieved by using the sliding mode controller of which a structure varies according to a pre-designed principle, so called the variable structure control. To compare this controller with another in robustness, PID controller for the same model of vehicle is designed. From various simulations for two controllers, it is shown that the sliding mode controller is the more robust anainst to modeling errors and disturbances.

전차륜 독립휠 구동 및 조향 제어 기반 특수목적용 6WD/6WS 차량의 주행제어 알고리즘 연구 (A Study on Maneuvering Control Algorithm Based on All-wheel Independent Driving and Steering Control for Special Purpose 6WD/6WS Vehicles)

  • 이대옥;여승태
    • 한국군사과학기술학회지
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    • 제16권3호
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    • pp.240-249
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    • 2013
  • This paper discusses the maneuvering control algorithm based on all-wheel independent driving and steering control techniques for special purpose 6WD/WS vehicles. The maneuvering control algorithms considering superior dynamic characteristics of high power in-wheel motors and independent steering system are designed to perform driving, steering, vehicle stability, and fault tolerant control. The maneuvering controller applies sliding and optimal control theories considering optimal torque distribution and friction circle related to the vertical tire force. The fault tolerant control algorithm is applied to obtain the similar maneuverability to that of the non-faulty vehicle. The simulations using the Matlab/Simulink dynamics model and experiments using HIL simulator mounting the real controllers with the designed control algorithms prove the improved performances in terms of vehicle stability and maneuverability.

선박조타의 TSK 퍼지 비선형제어시스템 설계 (Design of TSK Fuzzy Nonlinear Control System for Ship Steering)

  • 채양범;이원창;강근택
    • 한국항해항만학회지
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    • 제26권2호
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    • pp.193-197
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    • 2002
  • 선박 조종방정식의 비선형 요소를 고려한 선박의 자동조타시스템의 제어기를 설계하기 위하여 TSK (Takagj-Sugeno-Kang) 퍼지 이론을 이용하였다. TSK 퍼지모델은 비선형 시스템을 매우 효율적으로 표현할 수 있으며, 또 TSK 퍼지모델은 결론부가 선형식으로 이뤄져 있어 체계적인 제어기 설계가 가능하다. 따라서 본 연구에서는 선박의 조종방정식을 TSK 퍼지모델로 표현하는 방법과 그 모델로부터 체계적으로 TSK 퍼지제어기를 설계하는 방법을 설명한다.

해상 실측 자료를 이용한 횡동요 조종 계수 식별 (Parameter Identifications of Roll Maneuvering Coefficients Based on Sea Trial Data)

  • 김찬기
    • 대한조선학회논문집
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    • 제35권2호
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    • pp.29-37
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    • 1998
  • 물수체의 선형 운동방정식은 형상 설계와 제어기 설계의 지배방정식으로 사용되는 중요한 설계인자이다. 그러나, 경험식, 이론적 계산 및 모형 시험으로부터 획득한 운동방정식 내의 조종 계수들은 오차를 포함하고 있어 해상 시험을 동해 이에 대한 검증을 수행하여야 한다. 본 연구에서는 실측 자료에 대해 병렬 확장 칼만 필터, Nelder & Mead Simplex 탐색법 및 유전적 알고리즘을 적용하여 몰수체의 주요 횡 동요 계수들을 식별/비교하였다. 결론적으로 Nelder & Mead Simplex 탐색법이 사용된 수학 모형과 해상 시험 자료에 대해 가장 만족스런 결과를 주고 있다.

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모델 불확실성과 해파외란을 고려한 고려한 몰수체의 $H^{\inf}$ 제어기 설계 ($H^{\inf}$ controller design for submerged vehicle under model uncertainty and sea wave disturbances)

  • 이재명;류동기;이갑래;박홍배
    • 전자공학회논문지B
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    • 제33B권4호
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    • pp.17-26
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    • 1996
  • A submerged vehicle which is a nonlinear multivariable system must be designed to be roubst against inner-outer perturbations and hydrodynamic disturbances induces maneuvering operation. But a practical design of motion controller is limited by both mathematical modeling error and linearization errors. Performance of a motion controller based on traditional design method is very poor when the vehicle motion is under wave force distrubacnes near sea surface. Therefore, this ppaer proposes a design method of $^{\infty}$ controller under model uncertainty and sea wave disturbances. performance of the controllers by both computer simulation and HILS (hardwave in the loop simulation) shows that $H^{\infty}$ controller is more robust than PID controller under model uncertainty and high sea state...

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Optimal Control for Proximity Operations and Docking

  • Lee, Dae-Ro;Pernicka, Henry
    • International Journal of Aeronautical and Space Sciences
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    • 제11권3호
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    • pp.206-220
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    • 2010
  • This paper proposes optimal control techniques for determining translational and rotational maneuvers that facilitate proximity operations and docking. Two candidate controllers that provide translational motion are compared. A state-dependent Riccati equation controller is formulated from nonlinear relative motion dynamics, and a linear quadratic tracking controller is formulated from linearized relative motion. A linear quadratic Gaussian controller using star trackers to provide quaternion measurements is designed for precision attitude maneuvering. The attitude maneuvers are evaluated for different final axis alignment geometries that depend on the approach distance. A six degrees-of-freedom simulation demonstrates that the controllers successfully perform proximity operations that meet the conditions for docking.

Design of 6-DOF Attitude Controller of the UAV Simulator's Hovering Model

  • Keh, Joong-Eup;Lee, Mal-Young;Kim, Byeong-Il;Chang, Yu-Shin;Lee, Man-Hyung
    • 제어로봇시스템학회:학술대회논문집
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    • 제어로봇시스템학회 2004년도 ICCAS
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    • pp.969-974
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    • 2004
  • For a maneuvering unmanned autonomous helicopter, it is necessary to design a proper controller of each flight mode. In this paper, overall helicopter dynamics is derived and hovering model is linearized and transformed into a state equation form. However, since it is difficult to obtain parameters of stability derivatives in the state equation directly, a linear control model is derived by time-domain parametric system identification method with real flight data of the model helicopter. Then, two different controllers - a linear feedback controller with proportional gains and a robust controller - are designed and their performance is compared. Both proposed controllers show outstanding results by computer simulation. These validated controllers can be used to autonomous flight controller of a real unmanned model helicopter.

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