• Journal of Animal Science and Technology
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• 제66권2호
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• pp.295-309
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• 2024

To investigate the effect of dietary supplementation with a fermented mixture of bean dregs and wheat bran (FBW) on sow performance. FBW was given to sows during late gestation and lactation; in total, 24 sows were randomly assigned to 4 groups (control diet; 3% FBW diet; 6% FBW diet; 9% FBW diet, n = 6). The weight ratio of bean dregs (wet) to wheat bran was 4:6. Sows were fed different diets from 85 d of gestation until weaning. The results showed that supplementation with FBW increased average daily feed intake (ADFI) during lactation (p < 0.05). FBW supplementation also increased litter weight and milk yield (p < 0.05). The contents of Escherichia coli in the feces of the treatment groups were significantly reduced by FBW supplementation (p < 0.01). FBW supplementation significantly improved the fecal morphology (p < 0.05), alleviating sows' constipation. In conclusion, FBW could increase the ADFI, improve lactation and piglet litter weight in sows and reduce the pathogenic bacterial content in sow feces and constipation.

• 한국항공운항학회지
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• 제21권1호
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• pp.1-7
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• 2013

To have the competitiveness in the future worldwide small aircraft market, we should be able to develop the aircraft which is highly safe, easy to fly, and having excellent flight characteristics. FBW(Fly-By Wire) system is essential for the enhancement of flight safety and control easiness. FBW system that has been applied only to the modern fighter and transport aircraft is recently applied to smaller aircraft such as regional aircraft, business aircraft and even small aircraft. The purpose of this research includes the development of flight control computer, the definition of FBW system component, the design concept of each component for redundant management, OFP(Operational Flight Program) development, FBW system integration and HILS(Hardware In-the Loop Simulation) verification environment to test this FBW system.

• Asian Pacific Journal of Cancer Prevention
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• 제14권11호
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• pp.6321-6326
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• 2013

Introduction: Lung cancer is extremely harmful to human health and has one of the highest worldwide incidences of all malignant tumors. Approximately 80% of lung cancers are classified as non-small cell lung cancers (NSCLCs). Cisplatin-based multidrug chemotherapy regimen is standard for such lesions, but drug resistance is an increasing problem. F-box/WD repeat-containing protein 7 (FBW7) is a member of the F-box protein family that regulates cell cycle progression, and cell growth and differentiation. FBW7 also functions as a tumor suppressor. Methods: We used cell viability assays, Western blotting, and immunofluorescence combined with siRNA interference or plasmid transfection to investigate the underlying mechanism of cisplatin resistance in NSCLC cells. Results: We found that FBW7 upregulation significantly increased cisplatin chemosensitivity and that cells expressing low levels of FBW7, such as NCI-H1299 cells, have a mesenchymal phenotype. Furthermore, siRNA-mediated silencing or plasmid-mediated upregulation of FBW7 resulted in altered epithelial-mesenchymal transition (EMT) patterns in NSCLC cells. These data support a role for FBW7 in regulating the EMT in NSCLC cells. Conclusion: FBW7 is a potential drug target for combating drug resistance and regulating the EMT in NSCLC cells.

• 대한조선학회논문집
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• 제44권2호
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• pp.180-188
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• 2007

In this paper the longitudinal control problem for the large WIG(wing-in-ground effect) craft is considered in the sense of the control augmentation system(CAS) derived by control surface of elevator. In order to achieve longitudinally stable systems, two modes of CAS are applied to the control systems which are pitch rate hold mode and pitch hold mode for steady flight. Since the employed CASs include the dynamic properties of the actuator time delay and the low pass filter, it provides the possible solution to be applicable to real systems. Nonlinear model simulations are fulfilled to investigate the effectiveness of the applied CASs with wind disturbance.

• 한국통신학회논문지
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• 제32권11C호
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• pp.1095-1101
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• 2007

본 논문에서는 협대역 사용자와 스펙트럼을 공유하는 인지 라디오 시스템에서 협대역 간섭을 회피할 수 있도록 전체 TV 대역의 일부 대역을 가변적으로 사용하는 부분대역모드 기법을 소개한다. 이 때 동기 과정에서 바꿔 부분대역모드에 대한 정보를 얻을 수 있도록 프리앰블을 설계하고 부분대역모드 검출 기법을 포함한 시간 및 주파수 동기 알고리즘을 제안한다. 제안한 부분대역모드 검출 및 동기 성능을 WRAN (Wireless Regional Area Networks) 환경에서 모의 실험한 결과 동기 성능의 저하 없이 부분대역모드를 검출할 수 있음을 보인다.

• 한국항공우주학회지
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• 제41권6호
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• pp.488-494
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• 2013

전자식 비행제어시스템(Fly-By-Wire Flight Control System)에 적용되는 헬리콥터의 제어법칙 설계 및 해석은 모델기반 설계기법(Model Based Design)을 사용하여 개발되고 있다. 모델기반 설계기법은 회전익뿐만 아니라 고정익, 무인항공기, 자동차 산업에서도 널리 사용되고 있다. 모델기반 설계기법은 핵심기술인 시뮬레이션과 자동생성코드를 이용하여 개발기간 단축 및 개발리스크 감소라는 장점을 제공한다. 본 논문에서는 FBW 헬리콥터 비행제어법칙의 자동생성코드에 대해서 체계적인 기능검증을 위한 프로세스를 개발하였다. 그리고 지식경제부 과제로 진행하고 있는 FBW 헬리콥터 개발에 적용하여 비행제어법칙 자동생성코드의 기능 검증을 수행 결과, 요구 조건을 충족하는 것으로 확인할 수 있었다.

• 한국항공우주학회지
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• 제40권8호
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• pp.678-687
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• 2012

우천, 안개 낀 날씨 및 먼지 등에 의해 시계가 확보되지 않는 비행 환경에서의 헬리콥터의 안정성(stability) 및 비행성(flying quality)을 향상시키기 위해 모델 역변환 제어(Model Inversion Control) 방식의 전자식 비행제어시스템(Fly-By-Wire Flight Control System)의 적용은 필수적이다. 선진 항공사인 미국의 Bell-Sikorsky사와 유럽 컴소시움인 NHI(NH Industries)사는 FBW 비행제어시스템을 V-22와 NH-90의 헬리콥터 양산에 적용한 바 있다. 본 논문에서는 BO-105 모델을 기반으로 CONDUIT(Control Designer's Unified Interface)을 활용하여 제자리 비행영역에서 모델 역변환 비행제어법칙을 설계하였으며, 헬리콥터 비행조종성 국제규격인 ADS-33E-PRF을 기준으로 평가하였다. 설계된 비행제어법칙을 CONDUIT과 HETLAS(HElicopter Trim Linearization And Simulation)를 기반으로 평가한 결과, ADS-33E-PRF에서 제시하고 있는 예측 조종성(predicted handling quality) 규격에 대해 비행조종성 Level 1을 만족시킬 수 있었다.

• 항공우주시스템공학회지
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• 제3권3호
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• pp.32-38
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• 2009

An autothrottle module for small jet aircraft Fly-By-Wire system was developed. The autothrottle was designed to be composed of DC geared motor and electro-magnetic clutch that enables smooth manual/auto switching. A controller was designed for simple position control using ON/OFF control method with a commercial motor driver. The autothrottle developed was installed in the cockpit mockup and interfaced to the flight control computer for the HILS test. The performance test proved that the throttle lever follows well the command signal from the flight control computer.

• 한국해양공학회:학술대회논문집
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• 한국해양공학회 2000년도 춘계학술대회 논문집
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• pp.133-138
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• 2000

In this paper some shapes of the FBW cross sections were examined to improve the performance of FBW for the long wave. Trapezoidal section and prominence section were examined. Linear potential theory is used and the boundary element method is use for numerical computation. Proper choice of the pontoon geometry may improve the transmission coefficient in the long wave range for a given wave period.

• 항공산업연구
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• 통권53호
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• pp.95-104
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• 2000