• Title/Summary/Keyword: Design Verification

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Development of Electrical Power Subsystem of Cube Satellite STEP Cube Lab for Verification of Space-Relevant Technologies

  • Park, Tae-Yong;Chae, Bong-Geon;Oh, Hyun-Ung
    • International Journal of Aerospace System Engineering
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    • v.3 no.2
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    • pp.31-37
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    • 2016
  • STEP Cube Lab (Cube Laboratory for Space Technology Experimental Project) is a 1U standardized pico-class satellite. Its main mission objective is an on-orbit verification of five fundamental core space technologies. For assuring a successful missions of the STEP Cube Lab with five payloads, electrical power subsystem (EPS) shall sufficiently provide an electrical power to payloads and bus systems of the satellite during an entire mission life. In this study, a design process of EPS system was introduced including power budget analysis considering a mission orbit and various mission modes of the satellite. In conclusion, adequate EPS hardware in compliance with design requirements were selected. The effectiveness and mission capability of EPS architecture design were confirmed through an energy balance analysis (EBA).

Distributed and Real-time Integrated Simulation System on Avionics

  • Zhou, Yaoming;Liu, Yaolong;Li, Shaowei;Jia, Yuhong
    • International Journal of Aeronautical and Space Sciences
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    • v.18 no.3
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    • pp.574-578
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    • 2017
  • In order to achieve iterative design in early R&D period, a Distributed and Real-time Integrated Simulation System for avionics based on a Model-Based Systems Engineering (MBSE) method is proposed. The proposed simulation system includes driver, simulation model, monitor, flight visual model and aircraft external model.The effect of this simulation system in iterative design and system verification is testified by several use cases. The result shows that the simulation system, which can play an important role in iterative design and system verification, can reduce project costs and shorten the entire R&D period.

Multi type heat pump system computer simulation and experimental verification (멀티형 히트펌프 시스템 컴퓨터 시뮬레이션과 실험적 검증)

  • 한도영;정민영
    • Korean Journal of Air-Conditioning and Refrigeration Engineering
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    • v.12 no.1
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    • pp.12-19
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    • 2000
  • The multi type heat pump system may provide more energy savings and better environmental conditions than the single type heat pump system may do. In order to design a multi type heat pump system, it may be recommended to develop the system simulation program, which can predict the characteristics of the system such as unit capacities, power consumptions, and system COP's. In this study, the steady state simulation program of the multi type heat pump system was developed. The results from the simulation program were compared with those from the experimental tests which were performed in the environmental chamber, Cooling tests show 3.11% and 0.94% of error in capacity and COP, and heating tests show 3.30% and 1.90% of error in capacity and COP, respectively. Therefore, the steady state simulation program developed for this study can effectively be used for the design and the performance prediction of the multi type heat pump system.

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Design and Performance Verification of a LWIR Zoom Camera for Drones

  • Kwang-Woo Park;Jonghwa Choi;Jian Kang
    • Current Optics and Photonics
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    • v.7 no.4
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    • pp.354-361
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    • 2023
  • We present the optical design and experimental verification of resolving performance of a 3× long wavelength infrared (LWIR) zoom camera for drones. The effective focal length of the system varies from 24.5 mm at the wide angle position to 75.1 mm at the telephoto position. The design specifications of the system were derived from ground resolved distance (GRD) to recognize 3 m × 6 m target at a distance of 1 km, at the telephoto position. To satisfy the system requirement, the aperture (f-number) of the system is taken as F/1.6 and the final modulation transfer function (MTF) should be higher than 0.1 (10%). The measured MTF in the laboratory was 0.127 (12.7%), exceeds the system requirement. Outdoor targets were used to verify the comprehensive performance of the system. The system resolved 4-bar targets corresponding to the spatial resolution at the distance of 1 km, 1.4 km and 2 km.

Writer Verification Using Spatial Domain Features under Different Ink Width Conditions

  • Kore, Sharada Laxman;Apte, Shaila Dinkar
    • Journal of Computing Science and Engineering
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    • v.10 no.2
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    • pp.39-50
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    • 2016
  • In this paper, we present a comparative study of spatial domain features for writer identification and verification with different ink width conditions. The existing methods give high error rates, when comparing two handwritten images with different pen types. To the best of our knowledge, we are the first to design the feature with different ink width conditions. To address this problem, contour based features were extracted using a chain code method. To improve accuracy at higher levels, we considered histograms of chain code and variance in bins of histogram of chain code as features to discriminate handwriting samples. The system was trained and tested for 1,000 writers with two samples using different writing instruments. The feature performance is tested on our newly created dataset of 4,000 samples. The experimental results show that the histogram of chain code feature is good compared to other methods with false acceptance rate of 11.67%, false rejection rate of 36.70%, average error rates of 24.18%, and average verification accuracy of 75.89% on our new dataset. We also studied the effect of amount of text and dataset size on verification accuracy.

MIMO Antenna Design and Beam Pattern Verification for W-band Autonomous Driving Radar (W대역 자율주행 레이다용 MIMO 안테나 설계 및 빔 패턴 검증 방법)

  • Changhyun Lee;Junhyeok Choi;Milim Lee;Shinmyong Park;Seungyeol Baek
    • The Journal of the Institute of Internet, Broadcasting and Communication
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    • v.23 no.5
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    • pp.123-129
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    • 2023
  • MIMO antenna is a field in which various researches have been actively conducted for a long time, and its design concept is universally well known. However, Unlike conventional MIMO antennas, MIMO antennas for autonomous driving radars, which have recently been attracting attention, are designed in W-band which is a millimeter wave band, and must also meet novel design conditions to satisfy the performance of autonomous driving radars. Therefore, a novel and different approach is required for the design and beam pattern verification of the MIMO antenna for autonomous driving radar. In this paper, a MIMO antenna is designed and the design process to satisfy the conditions of a W-band autonomous driving radar is introduced, and proposes a beam pattern verification method for a W-band MIMO antenna mounted on an autonomous driving radar system.

Synthesized analysis and its verification of the piezoresistive pressure sensor (압저항형 압력센서의 통합해석 및 검증)

  • Yi, Seung-Hwan;Lee, Gon-Jae;Han, Seung-Oh
    • The Transactions of The Korean Institute of Electrical Engineers
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    • v.58 no.3
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    • pp.573-577
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    • 2009
  • Piezoresistive pressure sensor have become the successfully-commercialized MEMS product and the related technologies have been well developed over the past decades. Regarding the design methodology, however, the coupled-physics FEM analyses of the transducer itself and the signal-processing circuitry design based on the conventional EDA are separated and both of the analyses were sequentially processed for the full design of the pressure sensor. For the fast and effective R&D, new design methodology is proposed in this paper where the FEM results are linked to the EDA environment and therefore most of the design works can be done in the EDA environments, which means the time-consuming FEM analyses can be minimized. In order to verify the proposed approach, a typical piezoresistive pressure sensor having the silicon diaphragm and piezoresistors was modeled and analyzed based on the proposed methodology. The verification results showed that the simulated results were matched well with the measured data within the 7% difference while the simulation time was reduced less than 5% compared to the conventional methodology. Through the proposed approach, various types of the piezoresistive pressure sensors can be developed in more effective way.

A Study on the Consumer Behavior on Environmentally Beneficial Clothing (환경(環境) 친화적(親和的) 의류제품(衣類製品)에 대(對)한 소비자(消費者) 태도(態度)에 관(關)한 연구(硏究))

  • Lee, Ji-Eun;Kim, Il;Park, Sun-Kyung
    • Journal of Fashion Business
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    • v.6 no.2
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    • pp.77-92
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    • 2002
  • This study analyzed the consumer behavior on the environmentally Benefical clothing through the substantial verification, which was based on theoretical reviews. It also aimed to provided marketing aspects on the design, raw material, product quality, price, and brand recognition of environmentally Benefical clothing. For the substantial, verification following questions were developed. 1) Consumers' interests in purchasing environmentally Benefical clothing. 2) The consumer behavior on the environmental factors of the design, raw material, product quality, price, and brand recognition of environmentally Benefical clothing. 3) The changes in the consumer behavior on negative aspects of environmentally Benefical clothing. 4) The reasons of unfavorable behavior of environmentally unconscious consumers on environmentally Benefical clothing. Substantial data was collected through a survey, conducted on two hundreds and twenty-nine male and female students in graduate and undergraduate schools, resided in Seoul. The collected data was analyzed with Statistical Package for Social Science for Windows, version 8.0, and X2 and T-test were performed. Those results and issues, developed in the analysis of consumer behavior on the environmentally Benefical clothing, could be utilized in the environmental management and the marketing activity for the clothing companies.

Development of Propulsion Subsystem for KOMPSAST (다목적 실용위성의 추진시스템 개발)

  • 최진철;윤효철
    • Journal of the Korean Society of Propulsion Engineers
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    • v.2 no.3
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    • pp.80-89
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    • 1998
  • Propulsion subsystem transfers KOMPSAT into mission orbit and controls its attitude. Design factor consists of structure safety, electrical circuit design, consumable power estimation of thermal hardwares, damping device design of fuel transient pressure, and system configuration design by considering plume effect from thruster firing. System level analysis should be performed for verification of system design under launch vehicle and orbital environment. Electrical functional test of thermal control hardware, proof pressure test, cleanliness verification test, and internal/external leakage test of fuel feeding system should be carried out for performance estimation of propulsion system. Design and assembly process of propulsion subsystem was depicted and reliability of system was verified by test analysis in this paper.

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A Study on Development for Wind Turbine Rotor Hub using Design of Shape Optimization (형상 최적설계법을 이용한 풍력발전기 로터 허브 개발에 관한 연구)

  • Kim, Young-Il;Moon, Sung-Young;Lee, Ji-Hyun;Lee, Yun-Sung;Moon, Byung-Young
    • The KSFM Journal of Fluid Machinery
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    • v.14 no.3
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    • pp.59-64
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    • 2011
  • Wind turbine frame will be required to be longer, lighter, more reliable and more consistent. Therefore it is necessary to lose weight of the wind turbine hub. Light-weight Design of a wind turbine is required to be at least 20 years. Therefore, this paper investigates the development for wind turbine rotor hub using design of topology optimization. The model is a pitch regulated wind turbine with three rotor blades where the main frame is made of nodular iron. For optimization, calculating stresses based on displacements and based on these data to carry out a verification of static and fatigue strength carried out. For this verification, two kind of analysis is used. One is static analysis and the other is fatigue analysis. Then the rotor hub of wind turbine frame is optimized using topology method.