• 제목/요약/키워드: stick model

검색결과 188건 처리시간 0.025초

CIFER ® 를 이용한 무인 헬리콥터의 동특성 분석 (III) - 전달함수 해석 - (Flight Dynamic Identification of a Model Helicopter Using CIFER® (III) - Transfer Function Analysis -)

  • 배영환;구영모
    • Journal of Biosystems Engineering
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    • 제37권3호
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    • pp.192-200
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    • 2012
  • Purpose: Aerial application of chemicals with an agricultural helicopter allows for precise and timely spraying and reduces working labor and pollution. An attitude controller for an agricultural helicopter would be helpful to aerial application operator. The objectives of this paper are to determine the transfer function models and to estimate the handling qualities of a bare-airframe model helicopter. Methods: Transfer functions of a model unmanned helicopter were estimated by using NAVFIT and DERIVID modules of the $CIFER^{(R)}$ program to the time history data of frequency sweep flight tests. Control inputs of the transfer functions were elevator, aileron, rudder and collective pitch stick positions and the outputs were resulting on-axis movements of the fuselage. Results: Minimum realization of the transfer functions for pitch rate output to elevator control input and roll rate output to aileron control input produced second order transfer functions with undamped natural frequencies around 3.0 Hz and damping ratios of 0.139 and 0.530, respectively. The equivalent time delays of the transfer functions ranged from 0.16 to 0.44 second. Sensitivity analysis of the proposed parameters allowed derivation of minimal realization of the transfer functions. Conclusions: Handling quality of the model helicopter was addressed based on the eigenvalues of the transfer functions, corresponding undamped natural frequencies with damping ratios. The equivalent time delays of the lateral-directional motion ranged from 0.16 to 0.44 second, longer than the 0.1 to 0.15 second requirement for well-controlled typical manned aerial vehicles.

다중재질 접합구조의 등가물성을 이용한 효과적 냉장고 구조 변형 분석에 관한 연구 (Effective Analysis on the Mechanical Behavior of a Refrigerator using Equivalent Material Properties of Multi-layers)

  • 박정현;이동규;박상후;박기홍;하병국;김형식
    • 한국정밀공학회지
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    • 제29권11호
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    • pp.1228-1235
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    • 2012
  • A refrigerator has many components which are made from diverse materials such as metal, polymer, plastic, and rubber. So, it generally requires much time and efforts to build up an analysis model in finite element analysis. In this work, to reduce the computational time and efforts a simplified modeling method was proposed for the analysis of a refrigerator. Occasionally, a stick-slip noise occurs in a refrigerator due to relative slip between shelf and inner-case. When we solve the problem by a FE analysis, we should model the structures with detail for considering the contact conditions; by this reason, too many efforts are consumed in the conventional analysis method. Through this work, we shows the concept of simplifying approach and a good agreement with the results of a real model analysis. And also, the evaluation of the proposed method and the application of contact analysis using the simplified model are discussed.

홍대용이 제작한 천문시계 통천의의 기계동력시스템 (MECHANICAL POWER SYSTEM OF TONGCHEON-UI, AN ASTRONOMICAL CLOCK MADE BY HONG, DAE-YONG)

  • 민병희;윤용현;김상혁;기호철
    • 천문학논총
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    • 제35권3호
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    • pp.43-57
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    • 2020
  • Hong, Dae-Yong manufactured the Tongcheon-ui (Pan-celestial Armillary Sphere) with cooperating clock researcher Na, Kyeong-Jeok, and its craftsman An, Cheo-In, in Naju of Jeolla Province in 1760 ~ 1762. Tongcheon-ui is a kind of astronomical clock with an armillary sphere which is rotated by the force generated by a lantern clock's weight. In our study, we examine the lantern clock model of Tongcheon-ui through its description of the articles written by Hong himself. As his description, however, did not explain the detail of the mechanical process of the lantern clock, we investigate the remains of lantern clocks in the possession of Korea University Museum and Seoul National University Museum. Comparing with the clocks of these museums, we designed the lantern clock model of Tongcheon-ui which measures 115 mm (L) × 115 mm (W) × 307 mm (H). This model has used the structure of the striking train imitated from the Korea University Museum artifact and is also regulated by a foliot escapement which is connected to a going train for timekeeping. The orientation of the rotation of the going train and the striking train of our model makes a difference with the remains of both university museums. That is, on the rotation axis of the first gear set of Tongcheon-ui's lantern clock, the going and the striking trains take on a counterclockwise and clockwise direction, respectively. The weight of 6.4 kg makes a force driving these two trains to stick to the pulley on the twine pulling across two spike gears corresponding to the going train and the striking train. This weight below the pulley may travel down about 560 mm per day. We conclude that the mechanical system of Tongcheon-ui's lantern clock is slightly different from the Japanese style.

차체의 유연성을 고려한 고속철도 차량 승차감 해석 (Ride Comfort Analysis of High-Speed Train with Flexible Car Bodies)

  • 신범식;최연선;구자춘;이상원;이승일
    • 대한기계학회논문집A
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    • 제35권4호
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    • pp.341-346
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    • 2011
  • 고속철도 개발에 있어 승차감은 차량의 품질을 결정하는 중요한 요소이다. 본 논문에서는 고속철도 차량의 강체 및 유연체 모델 각각에 대해 속도증가에 따른 고속철도 차량의 승차감을 평가하였다. 가진원은 휠/레일 불균일에 의한 상하 진동만을 고려하였다. 속도 증가에 따른 차체의 진동을 계산하기 위해 강체 및 유연체 모델의 고유진동수와 모드형상을 계산하였다. 복잡한 형상의 압출재로 구성된 차체를 유연체로 모델링하기 위해 등가 물성치를 산출하여 등가 쉘로 모델링하였다. 계산된 차량의 진동으로 승차감을 평가한 결과, 강체 모델로 예측된 고속철도의 승차감은 고속에서 오히려 좋아지는 불합리한 결과가 도출 되었다. 반면 차량의 유연체 모드까지 고려하여 평가한 고속철도의 승차감은 속도 증가에 따라 승차감이 나빠지는 당연한 결과를 보여 주었다. 따라서 고속에서의 철도차량 개발은 차체의 유연체 특성을 고려해야함을 확인하였다.

곡률 커플링 접촉각에 따른 접촉 강성 및 굽힘 강성해석 (Analysis of Contact Stiffness and Bending Stiffness according to Contact Angle of Curvic Coupling)

  • 유용훈;조용주;이동현;김영철
    • Tribology and Lubricants
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    • 제34권1호
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    • pp.23-32
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    • 2018
  • Coupling is a mechanical component that transmits rotational force by connecting two shafts. Curvic coupling is widely used in high-performance systems because of its excellent power transmission efficiency and easy machining. However, coupling applications change dynamic behavior by reducing the stiffness of an entire system. Contact surface stiffness is an important parameter that determines the dynamic behavior of a system. In addition, the roughness profile of a contact surface is the most important parameter for obtaining contact stiffness. In this study, we theoretically establish the process of contact and bending stiffness analysis by considering the rough surface contact at Curvic coupling. Surface roughness parameters are obtained from Nayak's random process, and the normal contact stiffness of a contact surface is calculated using the Greenwood and Williamson model in the elastic region and the Jackson and Green model in the elastic-plastic region. The shape of the Curvic coupling contact surface is obtained by modeling a machined shape through an actual machining tool. Based on this modeling, we find the maximum number of gear teeth that can be machined according to the contact angle. Curvic coupling stiffness is calculated by considering the contact angle, and the calculation process is divided into stick and slip conditions. Based on this process, we investigate the stiffness characteristics according to the contact angle.

POTASSIUM REQUIREMENT OF MULE DUCKLINGS

  • Chu, C.L.;Wei, H.W.;Chen, B.J.;Shen, T.F.
    • Asian-Australasian Journal of Animal Sciences
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    • 제9권6호
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    • pp.643-646
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    • 1996
  • Experiments were conducted to determine potassium (K) requirement of mule ducklings. One-day-old ducklings with equal number of both sexes were fed diets containing graded levels of K for three weeks. In experiment 1, corn-soybean meal diet (CP 18.7%, ME 2,890 kcal/kg, K 0.80%) was used. The addition of K (0.00, 0.10, 0.20, 0.30, 0.40%) to the diet by potassium carbonate resulted in a decrease in weight gain and feed efficiency with the group fed on basal diet having the best performance. This means that the existing K in the basal diet is adequate for the growth of ducklings. In experiment 2, low K corn-isolated soy protein diet (K, 0.19%) was used. The supplementation of K (0.00, 0.16, 0.32, 0.48, 0.64%) resulted in an increase in weight gain and feed efficiency with the control group having the lowest performance. The minimum K requirement was found to be 0.49% for both maximum growth and best feed efficiency as determined by using bent-stick model.

A novel approach for the design of multi-class reentrant manufacturing systems

  • Yoo, Dong-Joon;Jung, Jae-Hak;Lee, In-Beum;Lee, Euy-Soo;Yi, Gyeong-beom
    • 제어로봇시스템학회:학술대회논문집
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    • 제어로봇시스템학회 2004년도 ICCAS
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    • pp.710-715
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    • 2004
  • The design problem of manufacturing system is addressed, adopting the closed queueing network model with multiple loops and re-entrant flows. The entire design problem is divided into two hierarchical sub-problems of (1) determining the station configuration and (2) optimizing the lot constitution; then they are tackled by neighbor search algorithm (NSA) and greedy mean value analysis (GMVA), respectively. Unlike the conventional MVA concerning multi-class closed queueing networks, the GMVA doesn't stick to a fixed lot proportion; rather it tries to find the optimal balance. The NSA, on the other hand, improves the object function value by altering the station configuration successively with its superior neighbor. The moderate time complexity, presented in big-${o}$ notation, enables us to apply the method even to the large-size practical cases, and the CPU time of an enlarged problem can be approximated by the same equation. The validity of our analytic approach is backed up by simulation studies with a widespread simulation package.

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중력 가속도로 인한 의식상실 감지 및 자동 회복 시스템 개발 (Development of Gravity-induced Loss of Consciousness(GLOC) Monitoring System and Automatic Recovery System)

  • 김종섭;황병문;강임주;장순용;김광윤;박명환
    • 제어로봇시스템학회논문지
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    • 제17권7호
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    • pp.704-713
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    • 2011
  • For many years, many pilots lost their lives and aircrafts due to GLOC(Gravity-induced Loss Of Consciousness). Due to the emergence of high-gravity maneuvering aircraft such as the F-16, F-15 and T-50, the automatic GLOC detection and recovery systems are necessary to increase the aircraft safeties even when the pilot loses his consciousness due to high-G maneuvering. This paper addresses the design of GLOC detection, warning and recovery algorithm based on a model of supersonic jet trainer. The system is solely controlled by the pilot's control input (i.e., control stick force) and aircraft status such as attitude, airspeed, altitude and so forth. And, moreover, it does not depend upon any pilot physiological condition. The test evaluation results show that the developed system supports the recovery of an aircraft from the unusual aircraft attitude and improves the aircraft safeties even when the pilot loses his consciousness due to high-G maneuvering.

Seismic modeling and analysis for sodium-cooled fast reactor

  • Koo, Gyeong-Hoi;Kim, Suk-Hoon;Kim, Jong-Bum
    • Structural Engineering and Mechanics
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    • 제43권4호
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    • pp.475-502
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    • 2012
  • In this paper, the seismic analysis modeling technologies for sodium-cooled fast reactor (SFR) are presented with detailed descriptions for each structure, system and component (SSC) model. The complicated reactor system of pool type SFR, which is composed of the reactor vessel, internal structures, intermediate heat exchangers, primary pumps, core assemblies, and core support structures, is mathematically described with simple stick models which can represent fundamental frequencies of SSC. To do this, detailed finite element analyses were carried out to identify fundamental beam frequencies with consideration of fluid added mass effects caused by primary sodium coolant contained in the reactor vessel. The calculation of fluid added masses is performed by detailed finite element analyses using FAMD computer program and the results are discussed in terms of the ways to be considered in a seismic modeling. Based on the results of seismic time history analyses for both seismic isolation and non-isolation design, the functional requirements for relative deflections are discussed, and the design floor response spectra are proposed that can be used for subsystem seismic design.

A method for earthquake response analysis of tall flexible structure

  • Liu, Tielin;Jiang, Yingchun;Luan, Yu
    • Earthquakes and Structures
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    • 제4권2호
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    • pp.133-155
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    • 2013
  • The earthquake responses are studied for the tall flexible structures such as TV towers when the vertical eccentricities between the discrete nodes and the corresponding centroids of investigated lumps are considered. In practical analyses, the tall flexible structures can be made into a spatial-discrete system of some certain length of beam elements with different lengths and cross-sectional areas. These elements are used to construct the investigated lumps in this paper. The different cross-sectional areas and the different lengths of two adjacent elements lead to the appearance of vertical eccentricity between the discrete node and the centroid of investigated lump within the same investigated lump. Firstly, the governing equations are established for a typical investigated lump. Secondly, the calculating formulae of the forces and moments acting on the investigated lump are derived and provided. Finally the new dynamic equilibrium equations with modified mass matrix and assemblage of stiffness matrix have been derived for the stick MDOF model based on beam theory when the existing vertical eccentricities are considered. Numerical results demonstrate that these vertical eccentricities should be considered in order to obtain the accurate earthquake responses for the tall flexible structures.