• Title/Summary/Keyword: 선회접근

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Docking Assessment Algorithm for AUVs with Uncertainties (불확실성이 포함된 무인잠수정의 도킹 평가 알고리즘)

  • Chon, Seung-jae;Sur, Joo-no;Jeong, Seong-hoon
    • Journal of Advanced Navigation Technology
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    • v.23 no.5
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    • pp.352-360
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    • 2019
  • This paper proposes a docking assessment algorithm for an autonomous underwater vehicles (AUVs) with sensor uncertainties. The proposed algorithm consists of two assessments, state assessment and probability assessment. The state assessment verifies the reachability by comparing forward distance to the docking station with expected distance to reach same depth as the docking station and necessity for correcting its route by comparing calculated inaccessible areas based on turning radius of the AUV to position of the docking station. When the AUV and the docking station is close enough and the state assessment is satisfied, the probability assessment is conducted by computing success probability of docking based on the direction angle, relative position to the docking station, and sensor uncertainties of the AUV. The final output of the algorithm is decided by comparing the success probability to threshold whether to try docking or to correct its route. To verify the validation of the suggested algorithm, the scenario that the AUV approaches to the docking station is implemented through Matlab simulation.

Structural Stability Evaluation for Special Vehicle Slewing Bearing using Finite Element Analysis (유한요소해석을 통한 특수차량용 선회베어링의 구조 안전성 평가)

  • Seo, Hyun-Soo;Lee, Ho-Jun;An, Tae-Su
    • Journal of the Korea Academia-Industrial cooperation Society
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    • v.22 no.1
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    • pp.511-519
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    • 2021
  • Slewing bearing is applied to the transmission of rotational power of the body and turret in a special vehicle for anti-aircraft weapons that overcomes the enemy flight system approaching at low altitudes with rapid response fire. When the turret load and impact load generated when shooting are combined in performing the combat mission of a special vehicle, structural stability must be secured to achieve a successful function. Among the components of the slewing bearing, the stability of the components against the complex loads acting by the turret drive and shooting was evaluated by considering the shape and material characteristics of the ring-gear, roller, and wire-race. As a research method for stability evaluation, based on engineering theory, the strength characteristics of the components were examined by numerical calculations. Finite element analysis was performed on components using the ANSYS analysis program. The results of theoretical analysis and the results of finite element analysis were very similar. A structural stability evaluation for the slewing bearing, which was performed mainly on the analysis, confirmed that the design strength of the slewing bearing determined in the preliminary design in the early stage of localization development was sufficient.

Application of GNSS Non-Precision and Precision Approaches to a Circle-to-Land Approach Airport (선회착륙공항에서의 GNSS 비정밀접근 및 정밀접근 적용 연구)

  • Kim, Y.M.;Kang, J.Y.
    • Journal of the Korean Society for Aviation and Aeronautics
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    • v.12 no.3
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    • pp.65-85
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    • 2004
  • Circling to land is a relatively dangerous maneuver. It contains the worst elements of IFR flight. There is a minimum obstruction clearance, a limited space in which to maneuver, an absence of visual reference, and trying to keep the runway in sight while preparing to land. At night it is quite a bit more than dangerous. The required continuous turn in marginal conditions that keeps the airport in sight is hazardous. Therefore, this paper proposes an application of GNSS to circling approach to reduce or remove chances of accidents which may occur under such unfavorable flight conditions. The study reviews relevant documents published by ICAO and FAA and provides scenarios for non-precision and precision approaches and circling approach based on the GNSS for Kimhae airport. Also requirements for the ground facility design are studied and provided.

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MANOEUVRABILITIES OF THE M.S. 'SAEBADA' ('새바다호의'의 조종성능에 관한 연구)

  • KIM Ki Yun
    • Korean Journal of Fisheries and Aquatic Sciences
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    • v.12 no.4
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    • pp.209-215
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    • 1979
  • The manoeuvrabilities of a ship are decided by the values of her manoeuvring indices. The manoeuvring indices consist of two kinds: indices K and T. The former decides a ship's turning ability and the latter, the length of time delay to a steady turning motion after her rudder has finished the turn of an ordered angle. In this paper, the author figured out the values of the manoeuvring indices of the m. s. 'SAEBADA' (GT: 2,275,7 ton), the training ship of tile National Fisheries University of Busan through her Z test and analyzed these values and the other data which were obtained from her Z test to study her manoeuvrabilities. The results of]tamed are summarized as follows: 1. The manoeuvring indices K' of the m. s. 'SAEBADA' were $1.052(at\;10{\circ}\;Z\;test)\;0.925(at\;20{\circ}\;Z\;test)\;and\;0.877(at\;30{\circ}\;Z\;test)$. Her manoeuvring indices $0.815(at\;10{\circ}\;Z\;test)\;0.502(at\;20{\circ}\;Z\;test)\;and\;0.441(at\;30{\circ}\;Z\;test)$. Her above calculated values K', T' showed that her obeying ability to the turn of her rudder was more increased when her rudder was used to large angle than to small angle, but on the other hand in this case her turning ability was slightly reduced. 2. As it appeared that the calculated K'-values of the m.s. 'SAEBADA' were slightly smaller than the standard K'-values of the fishing boats similar in length, and her overshoot angles at her Z test were greater than other general ships, her turning ability was found to t]e slightly lower. 3. When the m. s. 'SAEBADA' took a turn at her $10^{\circ}\;Z$ test, running distance was about 8.6 times her own length and didn't exceed the standard manoeuvrability distance, 5 to 11 times general ships' own length, therefore she was considered to have a good manoeuvrability synthetically.

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System Development Multidisciplinary Customized Learning and Evaluation Using the Mobile Web App (모바일 웹앱을 이용한 다학문 맞춤형 학습 및 평가 시스템 개발)

  • Jeong, Jae-Hoon;Kim, Sun-Hoi;Lee, Tae-Wuk
    • Proceedings of the Korean Society of Computer Information Conference
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    • 2013.01a
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    • pp.145-148
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    • 2013
  • 최근 디지털 기술의 고도화로 인하여 테크놀로지가 급속도록 발전하면서 다양한 정보통신 기술과 지식의 융합을 교육 환경에 적용하는 스마트러닝에 대한 관심이 집중되기 시작하였다. 이러한 스마트러닝 환경의 장점들을 통해 학생들이 더욱 효과적으로 교육받을 수 있게 되었다. 학생들은 모바일 기기의 접근성에 대한 인식이 확대되고 모바일 기기와 교육용 프로그램을 활용한 학습이 활성화 되고 있다. 이에 본 연구에서는 스마트기기를 이용한 학습과 평가가 이루어질 수 있는 방안에 대해 알아보고자 한다.

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Development of Dynamic Anlaysis Software for Rotor-Bearing Systems with Rotational Speed Depending Parameters (회전속도 의존매개변수를 갖는 회전체-베어링계의 동적해석프로그램 개발)

  • 장수현;이종원
    • Proceedings of the Korean Society for Noise and Vibration Engineering Conference
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    • 1991.04a
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    • pp.91-93
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    • 1991
  • DARBS는 저널베어링 및 구름베어링에 지지되어 있는 회전체-베어링계에 대한 동력학적 해석을 수행하는 프로그램이다. 해석에는 유한요소법(finite element method)을 이용하며 선회속도(whirl speed), 모우드 형성(mode shape), 임계속도(ciritical speed) 그리고 비동기 가진응답(asynchronous response)등에 대한 해석결과를 제공한다. 본 프로그램의 주된 특징은 람다 행렬(lambda matrices)의 개념을 도입하여 비동기 가진응답의 해석에 적용하 고, 베어링 상수와 자이로 효과와 같은 회전속도 의존성에 대하여 체계적인 접근방법을 사용했다는 점이다. 본 프로그램은 IBM PC 및 호환 기종에 적 합하도록 개발되었으며 기본적인 출력장치를 지원하는 S/W가 포함되어 있 다. 또한 대화식 데이타 입력과 메뉴처리방식을 채택하여 사용하기 편리하게 하였으며, 오류발생시 메세지가 나타나 오류수정을 용이하게 하였다.

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밀라노브리지 사고를 통해 본 프로펠러 벤틸레이션 현상 고찰

  • Gang, Seok-Yong;Lee, Yun-Seok
    • Proceedings of the Korean Institute of Navigation and Port Research Conference
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    • 2020.11a
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    • pp.72-74
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    • 2020
  • 일반적으로 선박조종에 필요한 중요한 성능으로 보침성능, 변침성능, 선회성능, 정지성능을 중요하게 여긴다. 이러한 조종성능은 선체의 선형과 함께 타와 엔진으로 표현될 수 있으며 특히 엔진의 성능은 선박의 안전운항과 직결되어 있다. 따라서 선박이 충분한 출력을 확보하지 못하면 항내조선시 선박의 안전을 담보하기 힘들며 또한 황천항해시 외력을 이기고 선박을 안전하게 조선하기 힘들다. 본 연구에서는 2020년 4월 6일 발생한 밀라노브릿지 사고를 통해 선박의 엔진출력을 저해하는 요소인 프로펠러 레이싱, 공전현상, 벤틸레이션 현상에 대하여 고찰하고자 하며 이를 통하여 선박의 조종성능에 미치는 출력을 중요성에 대하여 강조하고자 한다.

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Fabrication and Characteristics of CFRC(Carbon Firber Reinforced Carbon Composites) Fabricated with Carbon Fiber and Coal Tar Pitch Matrix (석탄계 핏치를 결합재로한 탄소/탄소 복합재의 제조 및 특징)

  • Ju, Hyeok-Jong;Choe, Don-Muk;O, In-Seok
    • Korean Journal of Materials Research
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    • v.4 no.2
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    • pp.194-205
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    • 1994
  • In this research, we attempt to fabricate an excellent CFRC(Carbon Fiber Reinforced Carbon), which has good thermal and mechanical properties, with 8H/satin woven fabric prepreg, high modulus and high strength type continuous carbon fiber and raw coal tar pitch(RCTP) matrix or THF soluble fraction(THFSP) matrix which has good graphitizability. Green bodies were fabricated with hot press molding technique and CFRC samples were made after carbonization, impregnation, recarbonization and graphitization steps. For the purpose of characterization of the physical properties, SEM, polarized light microscope, TGA were observed, and tested flexural strength, modulus and ILSS. After heat treating the THFSP matrix up to $2300^{\circ}C$, the value of $C_0$/2 was 3.380$\AA$, which is analogous to the structure of natural graphite and the value of 2$\theta$ is $26.276^{\circ}$ approached to the Bragg's angle of natural graphite. As a result of TGA to test the high temperature air oxidation, the THFSP matrix, graphitized up to $2300^{\circ}C$, exhibited the best air oxidation resistance. And mechanical properties were increased up to 65~70% as fiber volume fraction increased. Because of the good orientation graphitizability, the fracture surface of THFSP matrix CFRC is very good.

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Trend Analyses of B777 FLCH Usage Beyond FAF Events (B777 항공기 Final Approach Fix(FAF) 이후 Flight Level Change(FLCH) 사용 이벤트 경향성 분석)

  • Chung, Seung Sup;Kim, Hyeon Deok
    • Journal of Advanced Navigation Technology
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    • v.25 no.3
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    • pp.248-255
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    • 2021
  • The main causes of the July 2013 OZ 214 accident were poorly performed approach and the failure to recognize the autothrottle in the HOLD position which the automated speed control was not provided. The pilots late decision for go-around was also a critical factor leading to the accident. The B777 POM restricts the use of FLCH mode beyond the FAF. This research utilized the QAR data of an airline's B777 fleet in the period of two years where 44 cases were found. In many cases, the FLCH mode was used for rapid descent from an higher than normal situation. In addition, in the base turn, continuous use of FLCH mode even when the path was below the glide path were observed. Airports with elevation above 500 ft MSL had a higher rate of occurrence. In this research, the proper descent planning and vertical path monitoring, and the adherence to the limitation set in the manuals and the stabilized approach criteria were re-emphasized as mitigation to reduce event occurences.

Student's Conceptual Ecologies Concerning Motivational Beliefs and Socio-Cultural Values in the Context of General Chemistry Leanring (일반화학 학습의 맥락에서 동기적 신념과 사회-문화적 가치에 관한 개념생태의 범주)

  • Lee, Sun Kyung;Park, Hyun Ju;Kim, Uh Hee
    • Journal of the Korean Chemical Society
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    • v.44 no.3
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    • pp.266-280
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    • 2000
  • The purpose of this Study was to explore students' conceptual ecologies in the context of general chemistly learning. This study was implemented in the first semester of 1999 by natural study. We had nine voluntary participants. Data were collected from three semi-constructd interiews, and socio-cultural values. Among three categories, motivationa1 beliefs and socio-cultural values have more effcts rather than epistemology on the context of general chemistry learning, and three typical cases were presented as results of this study. We expect that results of this study will somewhat contribute to establish psychological and socio-cultural context of learning.

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