• 제목/요약/키워드: leader velocity

검색결과 17건 처리시간 0.019초

우두머리가 있는 두 생물무리의 가로지르기 동역학 (Crossing Dynamics of Leader-guided Two Flocks)

  • 이상희
    • 한국시뮬레이션학회논문지
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    • 제19권3호
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    • pp.37-43
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    • 2010
  • 우리는 두 생물무리가 서로 가로지르거나 결합하는 현상을 주변에서 흔히 볼 수 있다. 예로, 하천의 물고기 무리가 운동하다 바위나 돌같은 장애물을 만나 두 무리로 나누어졌다가 장애물 뒤에서 다시 하나로 합쳐지는 현상이 있다. 우두머리를 가지는 두 생물 무리가 각도${\theta}$를 가지고 서로 충돌하면서 가로질러 지나갈 때의 동역학을 연구하였다. 두 무리의 각 우두머리 개체는 다른 개체에 의해 영향을 받지 않는다. 이에 비해 무리의 개체들은 우두머리의 운동방향을 쫓아 가도록 시뮬레이션 되었다. 이 두 무리의 가로지르기 동역학을 이해하기 위해서, 무리개체의 평균 단위속도의 합으로 정의되는 질서매개변수${\phi}$를 조사하였다. 두 무리가 서로 만나는 순간, 두 무리의 운동량 균형이 무너지면서 ${\phi}$값이 급격히 올라갔다. 그리고 두 무리가 서로 분리되어질 때, 두 번째로 ${\phi}$값이 피크를 보였다. 무리개체들은 서로 충돌하면서 그들의 우두머리 개체를 쫓아가는데 방해를 받게 되는데 이로 인해 두 번째 피크이후에 불규칙적인 작은 피크들이 관측되었다. 두 피크값, $d_1$ (첫번째) 그리고 $d_2$ (두번째), 은 서로 다른 충돌각도 ${\theta}$에 대해서 동기화 현상을 보였다. 이 시뮬레이션 모델은 생물행동을 연구하거나 다개체 로봇 시스템 개발에 유용하게 사용되어 질수 있다.

Automatic Control for Chase Aircraft

  • Yamasaki, Takeshi;Enomoto, Keisuke;Tanaka, Daiki;Tanaka, Daiki;Baba, Yoriaki
    • International Journal of Aeronautical and Space Sciences
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    • 제7권2호
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    • pp.145-154
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    • 2006
  • Many kinds of unmanned aerial vehicles (UAVs) have been developed for a few decades and some of them are now in operational use. Although each UAV as well as a piloted aircraft might have restrictions to execute some tasks simultaneously or to carry some payloads, one with an automatic chase aircraft might have the potential of multi-capabilities to conduct a variety of missions or to carry more storages. This paper introduces a chase UAV control system to enhance a leader (reference) aircraft capability which has storage restriction. The automatic chase guidance and control system will be introduced with the pure pursuit guidance law combined with relative velocity error corrections, and a dynamic inversion technique in order to generate the guidance forces.

Controller Design using Sliding Mode Techniques for Satellite Formation Flying

  • Lim, Hyung-Chul;Bang, Hyo-Choong;Park, Kwan-Dong;Park, Pil-Ho;Jo, Jeong-Ho
    • 한국우주과학회:학술대회논문집(한국우주과학회보)
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    • 한국우주과학회 2003년도 한국우주과학회보 제12권2호
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    • pp.41-41
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    • 2003
  • Satellite formation flying is currently an active area of research in the aerospace engineering. There are many categories for this research such as the determination of initial conditions, formation keeping, configuration and reconfiguration. In this study, a tracking controller using sliding mode techniques is designed to control a satellite for the satellite formation flying. In general, Hill's equations are used to describe the relative motion of the follower satellite with respect to the leader satellite. But, the modified Hill's equations considering J2 perturbation were used for the design of sliding mode controller. Sliding mode control law causes the chattering phenomenon because it is a discontinuous control. Dead-zone was used to avoid the chattering. The Extended Kalman filter was applied to estimate the state vector based on the measurements of relative distance and velocity between two satellites.

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TRACKING CONTROL DESIGN USING SLIDING MODE TECHNIQUES FOR SATELLITE FORMATION FLYING

  • Lim, Hyung-Chul;Bang, Hyo-Choong;Park, Kwan-Dong;Park, Pil-Ho
    • Journal of Astronomy and Space Sciences
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    • 제20권4호
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    • pp.365-374
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    • 2003
  • Satellite formation flying is currently an active area of research in the aerospace engineering. So it has been researched by various authors. In this study, a tracking controller using sliding mode techniques was designed to control a satellite for the satellite formation flying. In general, Hill's equations are used to describe the relative motion of the follower satellite with respect to the leader satellite. However the modified Hill's equations considering the $J_2$ perturbation were used for the design of sliding mode controller. The extended Kalman filter was applied to estimate the state vector based on the measurements of relative distance and velocity between two satellites. The simulation results show that the follower satellite tracks the desired trajectory well by thruster operations based on the sliding mode control law.

두 시스템간의 편차 최소화를 적용한 상대적 동작제어 방법 (Relative Motion Control Methodology Using the Minimum Relative Error Between Two Systems)

  • 김성권
    • 제어로봇시스템학회논문지
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    • 제9권12호
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    • pp.994-1000
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    • 2003
  • A new relative motion control methodology for a following system to an independent leading system is proposed for controlling relative position, velocity, and tension etc. It is based on maintaining minimum relative error between two independent systems. The control command of the following system to a leading system is generated by adding the current command and the output of the relative error compensation. The proposed control method is implemented on the experimental equipment which is a wire winding-unwinding system to control the tension of the line. The results show the unwinding system(follower) following the independent motion of the winding system(leader) to control the constant tension of the line in order to keep the roller dancer in reference position. The relative motion control method proposed in this paper can be applied to high precision equipment for unwinding and winding fine wire, fine fiber, and tape etc.

이동물체 추적을 위한 이동로봇의 대형제어 (Formation Control of Mobile Robot for Moving Object Tracking)

  • 오영석;이충호;박종훈;김진환;허욱열
    • 전기학회논문지
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    • 제60권4호
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    • pp.856-861
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    • 2011
  • The mobile robot controller is designed to track the target and to maintain the formation at the same time. Formation control is included in mobile robot controller by extending the trajectory tracking algorithm. The dynamic model of mobile robot is used with kinematic model considering the practical physical parameters of mobile robot. The dynamic model of mobile robot transforms velocity control input of kinematic model into torque control input which is the practical control input of mobile robot. Formation controller of mobile robot is designed to satisfy Lyapunov stability by backstepping method. The designed formation controller is applied to the mobile robot for various target movements and simulated to confirm the Lyapunov stability.

Underwater Discharge Phenomena in Inhomogeneous Electric Fields Caused by Impulse Voltages

  • Lee, Bok-Hee;Kim, Dong-Seong;Choi, Jong-Hyuk
    • Journal of Electrical Engineering and Technology
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    • 제5권2호
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    • pp.329-336
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    • 2010
  • The paper describes the electrical and optical properties of underwater discharges in highly inhomogeneous electric fields caused by 1.2/50 ${\mu}s$ impulse voltages as functions of the polarity and amplitude of the applied voltage, and various water conductivities. The electric fields are formed by a point-to-plane electrode system. The formation of air bubbles is associated with a thermal process of the water located at the tip of the needle electrode, and streamer coronas can be initiated in the air bubbles and propagated through the test gap with stepped leaders. The fastest streamer channel experiences the final jump across the test gap. The negative streamer channels not only have more branches but are also more widely spread out than the positive streamer channels. The propagation velocity of the positive streamer is much faster than that of the negative one and, in fact, both these velocities are independent of the water conductivity; in addition the time-lag to breakdown is insensitive to water conductivity. The higher the water conductivity the larger the pre-breakdown energy, therefore, the ionic currents do not contribute to the initiation and propagation of the underwater discharges in the test conditions considered.