• Title/Summary/Keyword: MFD

Search Result 72, Processing Time 0.029 seconds

Computation Algorithm for Launch Acceptability Region of Air-to-Surface Missiles (공대지 유도탄의 발사유효범위(LAR) 산출 알고리듬)

  • Park, Sang-Sup;Hong, Ju-Hyeon;Ryoo, Chang-Kyung
    • Journal of the Korean Society for Aeronautical & Space Sciences
    • /
    • v.43 no.10
    • /
    • pp.910-919
    • /
    • 2015
  • A weapon control algorithm equipped on a fighter is closely related to the mission accomplishment and fighter survivability during the engagement. In the case of a air-to-surface missile, the weapon control algorithm typically provides a pilot the target shoot-down possible region known as launch acceptability region(LAR) in the multi function display(MFD). LAR is produced by the range table(RT) through computation of an engagement range. In this paper, the operation system of AGM-84 and AGM-88 air-to-surface missiles is introduced. And the engagement range computation and LAR algorithm based on the real-time pseudo 6-DOF simulation are proposed. In order to verify the performance of the algorithm, numerical engagement simulations of air-to-surface missiles to produce LAR have been done.

Buckling load optimization of laminated composite stepped columns

  • Topal, Umut
    • Structural Engineering and Mechanics
    • /
    • v.62 no.1
    • /
    • pp.107-111
    • /
    • 2017
  • This paper deals with critical buckling load optimization of symmetric angle-ply laminated stepped flat columns under axial compression load. The design objective is the maximization of the critical buckling load and the design variable is the fiber orientations in the layers of the laminates. The classical laminate plate theory is used for the finite element solution of the laminated stepped flat columns. The modified feasible direction (MFD) method is used for the optimization routine. For this purpose, a program based on FORTRAN is exploited. Finally, the optimization results are presented for width ratios (b/B), ratios of fillet radius ($r_1/r_2$), aspect ratios (L/B) and boundary conditions. The results are presented in graphical and tabular forms and the results are compared.

Implementation of Wide-Range Dimming Controller of LED Backlight for Avionics Displays (항공기 디스플레이용 LED Backlight의 광대역 Dimming Controller 구현)

  • Lim, S.H.;Lim, J.G.;Shin, H.B.;Chung, S.K.;Shin, M.J.;Sohn, S.G.
    • Proceedings of the KIPE Conference
    • /
    • 2007.11a
    • /
    • pp.53-55
    • /
    • 2007
  • This paper describes an implementation of a wide-range dimming controller of a LED backlight for Avionics applications such as the control data unit(CDU) and multi-function display(MFD). A feedback controller using a light sensor is proposed to control the brightness in the low dimming range. The proposed controller provides an improved control performance in the wide dimming range of 1:3000 even under the temperature variations. The experimental results are provided to show the effectiveness of the proposed control system.

  • PDF

Improved Mid P-value Method for Statistical Inference in Three-Way Contingency Tables

  • Donguk Kim
    • Communications for Statistical Applications and Methods
    • /
    • v.5 no.3
    • /
    • pp.905-926
    • /
    • 1998
  • We propose a modified mid P-value method to reduce the conservativeness for the inference of conditional associations in three-way contingency tables. This improves the ordinary mfd P-value method. For $2{\times} 2${\times} K$ tables, we propose confidence intervals for an assumed common odds ratio based on inverting two separate one-sided tests using the modified mid P-value. Also, an alternative and usually even better ways of constructing intervals, based on Inverting a two-sided test, are presented. The actual probability of coverage of a 100($1-\alpha$)% confidence interval is centered about the nominal level, but the modified mid P-value approach gives actual coverage probability even closer to the nominal level than the ordinary mid P-value approach.

  • PDF

Mirror Structure Analysis of High Resolution Optical Imaging Payload (고해상도 광학영상장비 반사경 구조해석)

  • Kwon, Woo-Gun;Kim, Kwang-Ro;Lee, Young-Shin
    • Proceedings of the KSME Conference
    • /
    • 2003.04a
    • /
    • pp.462-467
    • /
    • 2003
  • For the Space-borne optical imaging payload system design, light weighting and moderate stiffness of mirror and/or mirror fixation device is very important aspects. The front surface of mirror is regulated by optical performance requirement, but the shape of backplate of mirror is to be optimised while satisfing the required stiffness and weight. According to the results, the best shape of backplate cell is triangular. And also related geometric dimensions and the optimised mounting point of MFD(Mirror Fixation Device) is presented. Finally, natural frequencies and shpaes of mirror structure are analysed.

  • PDF

A Novel Architecture of UPnP Bridge for Non-IP devices (Non-IP 장치 제어를 위한 새로운 UPnP 브리지 구조)

  • Kang, Jeong-Seok;Choi, Yong-Soon;Kim, Seong-Hoon;Lee, Kwang-Koog;Park, Hong-Seong
    • Proceedings of the KIEE Conference
    • /
    • 2007.04a
    • /
    • pp.442-444
    • /
    • 2007
  • This paper presents an architecture of UPnP Bridge that allows controlling Non-iP devices from UPnP control point, without modification to Non-IP device or UPnP control point implementations. UPnP devices must provide SSDP discovery, SOAP control and GENA event processes. To represent Non-IP devices to UPnP devices, UPnP Bridge provides these functionalities on behalf of Non-IP devices. We provides two method to interoperability between UPnP and Non-IP devices, Message Field Description, Non-UPnP Proxy devices. And solution to integrate heterogeneous networking standards(RS232C, CAN, IEEE1394, USB) is provided.

  • PDF

A Real-Time NDGPS/INS Navigation System Based on Artificial Vision for Helicopter (인공시계기반 헬기용 3차원 항법시스템 구성)

  • Kim, Jae-Hyung;Lyou, Joon;Kwak, Hwy-Kuen
    • Journal of the Korea Institute of Military Science and Technology
    • /
    • v.11 no.3
    • /
    • pp.30-39
    • /
    • 2008
  • An artificial vision aided NDGPS/INS system has been developed and tested in the dynamic environment of ground and flight vehicles to evaluate the overall system performance. The results show the significant advantages in position accuracy and situation awareness. Accuracy meets the CAT-I precision approach and landing using NDGPS/INS integration. Also we confirm the proposed system is effective enough to improve flight safety by using artificial vision. The system design, software algorithm, and flight test results are presented in details.

The Model Driven Development of the Multi-function Display Software for Avionics (모델 기반 항공기 다중 시현기 소프트웨어의 개발)

  • Yoo, Hongseok;Hwang, Dong Gil;Kim, So Yong;Park, Ye Chan;Park, Seong Hun
    • Proceedings of the Korean Society of Computer Information Conference
    • /
    • 2017.07a
    • /
    • pp.413-414
    • /
    • 2017
  • 항공전자 시스템 및 소프트웨어 기술의 복잡성이 증가함에 따라 소프트웨어의 신뢰성을 보장하는 방법으로 모델 기반 소프트웨어 개발의 필요성이 증가하고 있다. 본 논문에서는 모델기반 소프트웨어 설계를 이용하여 항공기 콕핏 내 주요 계기를 통합한 MFD(Multi-function Display)를 설계하고, 실시간 비행 데이터를 생성하여 시뮬레이션한 결과를 보인다.

  • PDF

ACROFACIAL DYSOSTOSIS : A CASE REPORT (사지안면골형성부전증(Acrofacial Dysostosis) 환자의 증례보고)

  • Lee, Byeong-Do
    • Maxillofacial Plastic and Reconstructive Surgery
    • /
    • v.21 no.2
    • /
    • pp.220-224
    • /
    • 1999
  • The acrofacial dysostosis(AFD) is a rare heterogenous disorders combining varying severities of mandibulofacial dysostosis(MFD) with pre and/or post axial limb abnormalities. The Nager syndrome is characterized by preaxial limb defects whereas Miller syndrome is characterized by post axial limb defects. Our AFD case is a 14-year old female. She showed malar hypoplasia, cleft lip & palate(Rt, Lt side), wide nasal bridge, telecanthus. Her right thumb was abscent and middle phalanx, radius, carpal bones of right hand were hypoplastic, and metatarsus varus was present. She showed normal stature and intelligence.

  • PDF

Thermal buckling load optimization of laminated plates with different intermediate line supports

  • Topal, Umut
    • Steel and Composite Structures
    • /
    • v.13 no.3
    • /
    • pp.207-223
    • /
    • 2012
  • This paper deals with critical thermal buckling load optimization of symmetrically laminated four layered angle-ply plates with one or two different intermediate line supports. The design objective is the maximization of the critical thermal buckling load and a design variable is the fibre orientation in the layers. The first order shear deformation theory and nine-node isoparametric finite element model are used for the finite element solution of the laminates. The modified feasible direction (MFD) method is used for the optimization routine. For this purpose, a program based on FORTRAN is used. Finally, the numerical analysis is carried out to investigate the effects of location of the internal line supports, plate aspect ratios and boundary conditions on the optimal designs and the results are compared.