• Title/Summary/Keyword: 조종성능 추정

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A Study on a Small Canard Aircraft Flight Characteristics through Flight Test (비행시험을 통한 소형 커나드항공기의 비행 특성 연구)

  • Kim, Eung-Tai;Seong, Kie-Jeong
    • Journal of the Korean Society for Aeronautical & Space Sciences
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    • v.30 no.6
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    • pp.31-38
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    • 2002
  • This paper presents the analysis of the flight test data measured by the sensors installed on a four-seat canard aircraft. The inherent stall proof characteristics of canard aircraft was verified from the stall test. The dihedral effect, adverse yaw and roll control power were examined and the neutral point that determines the longitudinal stability of the aircraft was investigated. The dynamic characteristics such as dutch roll mode were also examined. Without relying on the parameter identification method, the aerodynamic derivatives or the relations between the aerodynamic derivatives were obtained by analyzing the steady state flight data.

Estimation of Hydrodynamic Derivatives of Submarine Model by Using VPMM Test (VPMM 시험을 이용한 잠수함 모형의 유체력 미계수 추정)

  • Jung, Jin-Woo;Jeong, Jae-Hun;Kim, In-Gyu;Lee, Seung-Keon
    • Journal of Navigation and Port Research
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    • v.38 no.2
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    • pp.97-103
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    • 2014
  • In these days, the world has been increasing navy forces such as aircraft carriers and high-tech destroyers etc. and the importance of submarines is being emphasized. Therefore, accurate values of the derivatives in equations of motion are required to control motion of the submarines. Hydrodynamic derivatives were measured by the vertical planar motion mechanism(VPMM) model test. VPMM equipment gave pure heave and pitch motion respectively to the submarine model and the forces and moments were acquired by load cells. As a result, the hydrodynamic derivatives of the submarine are provided through the Fourier analysis of the forces and moments in this paper.

Study on the Course Stability of a Barge in Waves (파랑중 부선의 침로안정성에 관한 연구)

  • Lee, Sangmin
    • Journal of the Korean Society of Marine Environment & Safety
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    • v.24 no.4
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    • pp.430-437
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    • 2018
  • For a ship navigating in waves, added resistance, sway force and yaw moment due to waves differ from still water conditions, which affects the maneuverability of the ship. Therefore, it is important to estimate the sway force and yaw moment generated by waves. In this study, numerical simulations were carried out to calculate the hydrodynamic forces acting on a barge in still water and waves using CFD. Based on the results, the characteristics of course stability of a barge were investigated and analyzed. The hydrodynamic forces acting on the barge in waves were stronger than in still water, and it was confirmed that hydrodynamic forces become greater as wavelength becomes longer. In long wavelength regions, the (-) value of the yaw damping lever was larger than in still water. However, in short wavelength regions and when wavelength coincided with the length of the ship, values were smaller than in still water. In this region, it can be assumed that course stability improved. In other words, in long wavelength regions, the course stability of the barge was worse than in still water and short wavelength regions. Therefore, attention is required for safe navigation in long wavelength regions.

Prediction of Maneuverability of a Submarine at Surface Condition by Captive Model Test (구속모형시험을 통한 잠수함 선형의 수상 조건 조종성능 추정 연구)

  • Chang-Seop, Kwon;Dong-Jin, Kim;Young-Yeon, Lee;Yeon-Gyu, Kim;Kunhang, Yun;Sungrok, Cho
    • Journal of the Society of Naval Architects of Korea
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    • v.59 no.6
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    • pp.423-431
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    • 2022
  • In this paper, the results of Planar Motion Mechanism (PMM) test for a 1/15 scaled model of the MARIN Joubert BB2 submarine is dealt with to derive the maneuvering coefficients for surface condition. For the depth of surface navigation, the top of the sail was exposed 0.46 m above the water surface in the model scale, and it corresponds to 6.9 m in the full scale. The resistance and self-propulsion tests were conducted, and the model's self-propulsion point was obtained for 1.328 m/s, which corresponded to 10 knots in the full scale. The maneuvering tests were performed at the model's self-propulsion point, and the maneuvering coefficients were obtained. Based on the maneuvering coefficients, a turning simulation was performed for starboard 30 degree of stern fins. The straight-line stability and control effectiveness in the horizontal plane were analyzed using the maneuvering coefficients and compared with the appropriate range. For the analysis of the neutral fin angle of the X-type stern fin, the stern fin test with drift angles was carried out. As a result, the flow straightening effect at lower and upper parts of the stern fin was discussed.

Effect of a Gap of a 2-D Flap Rudder on the Lift (2차원 플랩타의 간극이 양력에 미치는 영향)

  • Chang-Gu Kang
    • Journal of the Society of Naval Architects of Korea
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    • v.30 no.4
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    • pp.31-38
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    • 1993
  • Horn rudders or flap rudders with a gap between forward and after part are used for effective steering of a ship or a submerged body. It is necessary to analyze the effect of a gap since it affects the performance of rudders. In this paper, an equation to calculate the lift acting on a two-dimensional flap rudder in uniform flow is derived by using the thin hydrofoil theory and the analytic solution of viscous flow in a channel formed by two coaxial cylindrical walls to which a pressure gradient is applied.

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Sensorless BLDC Motor Control to Drive Fins for Flight Attitude Control of a Guided Artillery Munition (유도형 탄약의 조종날개 제어용 Sensorless BLDC 전동기 구동시스템 개발)

  • Kim, Sang-Hoon;Lee, Tae-Hyung;Cho, Chang-Yeon;Pak, Chang-Ho;Kim, Jae-Ho
    • Proceedings of the KIPE Conference
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    • 2014.07a
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    • pp.49-50
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    • 2014
  • 본 논문에서는 유도형 활공 탄약의 비행경로 제어와 자세유지를 위해 장착된 꼬리 날개 구동을 위한 BLDC 전동기 제어시스템을 개발하였다. 이 시스템에서는 높은 고도에서의 비행 시 압력에 취약한 홀(Hall) 센서와 같은 회전자의 위치 검출 센서를 사용하지 않는 센서리스(Sensorless) 구동 방식을 적용하였다. 측정된 극전압으로부터 상전환 신호를 추출하여 BLDC 전동기의 센서리스 구동을 실현하였으며, 또한 상전환 신호로부터 추정된 속도를 사용하여 속도 제어를 통해 꼬리날개의 변위 명령 추종을 위한 위치 제어를 수행하였다. 실제 구현된 시스템에서의 실험을 통해 개발된 센서리스 제어 알고리즘을 적용하여 위치 제어의 성능이 우수함을 확인하였다.

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Estimation of maneuvering characteristic of training ship Baek-Kyung according to water depth (수심에 따른 실습선 백경호의 조종성능 추정)

  • Chun-Ki LEE;Kyung-Jin RYU;Yoo-Won LEE;Su-Hyung KIM
    • Journal of the Korean Society of Fisheries and Ocean Technology
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    • v.59 no.3
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    • pp.261-263
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    • 2023
  • Recently, universities of fisheries and institutions related to fisheries are actively carrying out a project to build new fisheries training ships. These new fisheries training ships are significantly larger in size and longer in length than the previous ships. In addition, these new ships basically have space that can accommodate more than 100 crew and passenger. On the other hand, they are excluded from IMO maneuverability evaluation since the size of these ships are still less than 100 m in length (LBP). These results have had an impact on the study of maneuverability of fishing vessels including the fisheries training ships. Against these backgrounds, the authors conducted a study to estimate the maneuvering characteristics of fisheries training ship Baek-Kyung according to depth in order to prepare a maneuvering characteristic index that enables the large fisheries training ships to navigate more safely using a modified empirical formula. It was confirmed that the maneuvering characteristics of Baek-Kyung changed significantly as the values of the hydrodynamic force coefficients changed as the water depth gradually decreased from around 1.5 (approx. 8 m in depth) of the ratio of the water depth to the ship draft. The results of this study will not only help navigators understand the maneuvering characteristics of Baek-Kyung, but also serve as an indicator when navigating in shallow water. In addition, the accumulation of these results will serve as a basis for future study on maneuverability of fishing vessel types.

Stability Analysis of Missiles with Strapdown Seeker (스트랩다운 탐색기를 탑재한 유도탄의 안정성 해석)

  • Kim, Tae-Hun;Park, Bong-Gyun;Kwon, Hyuck-Hoon;Kim, Yoon-Hwan;Tahk, Min-Jea
    • Journal of the Korean Society for Aeronautical & Space Sciences
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    • v.39 no.4
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    • pp.332-340
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    • 2011
  • A missile with a strapdown seeker should properly estimate line-of-sight(LOS) rate using its attitude information and the look angle of the seeker because LOS rate information in an inertial coordinate system, which is used for a proportional navigation(PN) homing guidance, can not be obtained directly. However, an unnecessary feedback loop(Parasite Loop) is formed in the guidance and control loop, and it may cause the guidance performance degradation or even the unstability of the system(Parasite Effect). This paper presents estimation methods for the LOS rate information and effective ways to minimize the parasite effect using Routh-Hurwitz stability criterion. Various numerical simulations are also included to verify the proposed methods.

Effect of Wind Speed Profile on Wind Loads of a Fishing Boat (풍속 분포곡선이 어선의 풍하중에 미치는 영향에 관한 연구)

  • Lee, Sang-Eui
    • Journal of the Korean Society of Marine Environment & Safety
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    • v.26 no.7
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    • pp.922-930
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    • 2020
  • Marine accidents involving fishing boats, caused by a loss of stability, have been increasing over the last decade. One of the main reasons for these accidents is a sudden wind attacks. In this regard, the wind loads acting on the ship hull need to be estimated accurately for safety assessments of the motion and maneuverability of the ship. Therefore, this study aims to develop a computational model for the inlet boundary condition and to numerically estimate the wind load acting on a fishing boat. In particular, wind loads acting on a fishing boat at the wind speed profile boundary condition were compared with the numerical results obtained under uniform wind speed. The wind loads were estimated at intervals of 15° over the range of 0° to 180°, and i.e., a total of 13 cases. Furthermore, a numerical mesh model was developed based on the results of the mesh dependency test. The numerical analysis was performed using the RANS-based commercial solver STAR-CCM+ (ver. 13.06) with the k-ω turbulent model in the steady state. The wind loads for surge, sway, and heave motions were reduced by 39.5 %, 41.6 %, and 46.1 % and roll, pitch, and yaw motions were 48.2 %, 50.6 %, and 36.5 %, respectively, as compared with the values under uniform wind speed. It was confirmed that the developed inlet boundary condition describing the wind speed gradient with respect to height features higher accuracy than the boundary condition of uniform wind speed. The insights obtained in this study can be useful for the development of a numerical computation method for ships.

Intelligent Maneuvering Target Tracking Based on Noise Separation (잡음 구분에 의한 지능형 기동표적 추적기법)

  • Son, Hyun-Seung;Park, Jin-Bae;Joo, Young-Hoon
    • Journal of the Korean Institute of Intelligent Systems
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    • v.21 no.4
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    • pp.469-474
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    • 2011
  • This paper presents the intelligent tracking method for maneuvering target using the positional error compensation of the maneuvering target. The difference between measured point and predict point is separated into acceleration and noise. K-means clustering and TS fuzzy system are used to get the optimal acceleration value. The membership function is determined for acceleration and noise which are divided by K-means clustering and the characteristics of the maneuvering target is figured out. Divided acceleration and noise are used in the tracking algorithm to compensate computational error. While calculating expected value, the non-linearity of the maneuvering target is recognized as linear one by dividing acceleration and the capability of Kalman filter is kept in the filtering process. The error for the non-linearity is compensated by approximated acceleration. The proposed system improves the adaptiveness and the robustness by adjusting the parameters in the membership function of fuzzy system. Procedures of the proposed algorithm can be implemented as an on-line system. Finally, some examples are provided to show the effectiveness of the proposed algorithm.