• Title/Summary/Keyword: Way-Point 추종 시뮬레이션

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Development & Test of A Small-Sized Autonomous Underwater Vehicle "BOTO" (소형 자율무인잠수정 "BOTO"의 개발 및 실험)

  • Byun, Seung-Woo
    • Journal of the Institute of Electronics and Information Engineers
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    • v.49 no.11
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    • pp.103-109
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    • 2012
  • Samsung Thales has developed a small-sized autonomous underwater vehicle "BOTO" verified by a mathematical model simulation. The hydrodynamic coefficients and drag force were experimented at circulating water channel for validating cruising performance of the AUV. Based on the mathematical model, we simulated turning radius and way-point tracking on horizontal plane using way-point tracking algorithm. In this paper we introduce the vehicle system and the sea trial test results will be shown.

A Comparative Study on Guidance Systems for Ship's Track-Keeping (선박의 항로추종 유도기법에 관한 비교 연구)

  • Xu, Zhizun;Kim, Heon-Hui;Park, Gyei-Kark;Nam, Taek-Kun
    • Proceedings of the Korean Institute of Navigation and Port Research Conference
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    • 2016.05a
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    • pp.308-309
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    • 2016
  • This paper deals with ship's track keeping methods which is crucial part of automatic navigation control systems. In this paper, we mainly discuss the performance of different guidance methods including way point guidance, enclosure-based steering guidance and lookahead-based steering guidance system. As a controller, a PID control system is employed to control ship's rudder angle during track-keeping. Finally, the performance of three methods are discussed through some simulation results.

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Flight Control of Tilt-Rotor Airplane In Rotary-Wing Mode Using Adaptive Control Based on Output-Feedback (출력기반 적응제어기법을 이용한 틸트로터 항공기의 회전익 모드 설계연구)

  • Ha, Cheol-Keun;Im, Jae-Hyoung
    • Journal of the Korean Society for Aeronautical & Space Sciences
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    • v.38 no.3
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    • pp.228-235
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    • 2010
  • This paper deals with an autonomous flight controller design problem for a tilt-rotor aircraft in rotary-wing mode. The inner-loop algorithm is designed using the output-based approximate feedback linearization. The model error originated from the feedback linearization is cancelled within allowable tolerance by using single-hidden-layer neural network. According to Lyapunov direct stability theory, the adaptive update law is derived to run the neural network on-line, which is based on the linear observer dynamics. Moreover, the outer-loop algorithm is designed to track the trajectory generated from way-point guidance. Especially, heading and flight-path angle line-of-sight guidance are applied to the outer-loop to improve accuracy of the landing tracking performance. The 6-DOF nonlinear simulation shows that the overall performance of the flight control algorithm is satisfactory even though the collective input response shows instantaneous actuator saturation for a short time due to the lack of the neural network and the saturation protection logic in that loop.

Motion Performance Prediction and Experiments of an Autonomous Underwater Vehicle through Fluid Drag Force Calculations (유체항력 계산을 통한 자율무인잠수정의 운동성능 예측과 실험)

  • Kim, Chang Min;Baek, Woon Kyung
    • Journal of Advanced Marine Engineering and Technology
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    • v.39 no.6
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    • pp.614-619
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    • 2015
  • In this study, a dynamics model was developed to predict the motion performance of an Autonomous Underwater Vehicle (AUV). The dynamics model includes basic dynamic state variables of the hull and force terms to determine the motion of the AUV. The affecting terms for the forces are hydrostatic force, added mass, hydrodynamic damping, lift and drag forces. The force terms can be calculated using analytical and Computational Fluid Dynamics methods. For the underwater motion simulation, a simple PD controller was used. Also, the AUV was tested in a water tank and near sea for the partial verification of the fluid drag force coefficients and way-point tracking motions.

Study on a Navigated Simulator of the Underwater Cleaning Robot (수중청소로봇의 운항 제어용 시뮬레이터 연구)

  • Choi, Hyeung-Sik;Kang, Jin-Il;Hong, Sung-Yul;Park, Han-Il;Seo, Joo-No;Kim, Moon-Hwan;Gwon, Kyeong-Yeop
    • Journal of Navigation and Port Research
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    • v.33 no.6
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    • pp.387-393
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    • 2009
  • In this paper, a 3-D simulator was developed to estimate visually the performance of propelling and integrated control system of the underwater cleaning robot. Based on the dynamics analysis of the UCR, the 3-D model of the UCR was used in the simulator in which position and velocity are included Also, an input and control system using a joystick was developed, and the simulator was applied to the input and control of the simulator. Moreover, an integrated navigation control system was designed, and its performance was validated by a way-point simulator including a PI-based fuzzy control law.

Study on a Limit MPPT Controller for the Modelling of a Wind Power Generator (풍력발전기 모델링 및 리미트 MPPT제어기에 관한 연구)

  • Kang, Ju-Sung;Koh, Kang-Hoon;Choi, Kwang-Ju;Park, Jae-Yoon
    • Journal of the Korean Institute of Illuminating and Electrical Installation Engineers
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    • v.21 no.5
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    • pp.53-59
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    • 2007
  • Now, the study is activity that the energy market depending on a fossil fuel tend to change different way. In middle of the study compositive use of renewable energy(fuel cell and wind power, solar cell, etc.) is dispersion power system which concern is increasing. But in the case of generation of electric wind power system is changeable to be turbulence and wind and win speed are changeable in several seconds, so making the best of wind energy the MPPT that role in this case is important. In this paper suggest a MPPT which is making a use of information of wind speed and turning speed, windmill, electric power but it is simpler than former way. We could verify that a proposed controller working at the highest point of electric power when wind speed is regular speed and changable speed through the simulation.

Control Law Design for a Tilt-Duct Unmanned Aerial Vehicle using Sigma-Pi Neural Networks (Sigma-Pi 신경망을 이용한 틸트덕트 무인기의 제어기 설계연구)

  • Kang, Youngshin;Park, Bumjin;Cho, Am;Yoo, Changsun
    • Journal of Aerospace System Engineering
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    • v.11 no.1
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    • pp.14-21
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    • 2017
  • A Linear parameterized Sigma-Pi neural network (SPNN) is applied to a tilt-duct unmanned aerial vehicle (UAV) which has a very large longitudinal stability ($C_{L{\alpha}}$). It is uncontrollable by a proportional, integral, derivative (PID) controller due to heavy stability. It is shown that the combined inner loop and outer loop of SPNN controllers could overcome the sluggish longitudinal dynamics using a method of dynamic inversion and pseudo-control to compensate for reference model error. The simulation results of the way point guidance are presented to evaluate the performance of SPNN in comparison to a PID controller.