• Title/Summary/Keyword: Aircraft equipment

Search Result 328, Processing Time 0.028 seconds

The comparative study of PKNU2 Image and Aerial photo & satellite image

  • Lee, Chang-Hun;Choi, Chul-Uong;Kim, Ho-Yong;Jung, Hei-Chul
    • Proceedings of the KSRS Conference
    • /
    • 2003.11a
    • /
    • pp.453-454
    • /
    • 2003
  • Most research materials (data), which are used for the study of digital mapping and digital elevation model (DEM) in the field of Remote Sensing and Aerial Photogrammetry are aerial photographs and satellite images. Additionally, they are also used for National land mapping, National land management, environment management, military purposes, resource exploration and Earth surface analysis etc. Although aerial photographs have high resolution, the data, which they contain, are not used for environment exploration that requires continuous observation because of problems caused by its coastline, as well as single - spectral and long-term periodic image. In addition to this, they are difficult to interpret precisely because Satellite Images are influenced by atmospheric phenomena at the time of photographing, and have by far much lower resolution than existing aerial photographs, while they have a great practical usability because they are mulitispectral images. The PKNU 2 is an aerial photographing system that is made to compensate with the weak points of existing aerial photograph and satellite images. It is able to take pictures of very high resolution using a color digital camera with 6 million pixels and a color infrared camera, and can take perpendicular photographs because PKNU 2 system has equipment that makes the cameras stay level. Moreover, it is very cheap to take pictures by using super light aircraft as a platform. It has much higher resolution than exiting aerial photographs and satellite images because it flies at a low altitude about 800m. The PKNU 2 can obtain multispectral images of visible to near infrared band so that it is good to manage environment and to make a classified diagram of vegetation.

  • PDF

Research about Multi-spectral Photographing System (PKNU No.2) Development (다중영상촬영을 위한 PKNU 2호 개발에 관한 연구)

  • 최철웅;김호용;전성우
    • Korean Journal of Remote Sensing
    • /
    • v.19 no.4
    • /
    • pp.291-305
    • /
    • 2003
  • The cost of deploying Geological and Environmental information gathering systems, especially when such systems obtain remote sensing and photographic data through the use of commercial satellites and aircraft. Besides the high cost equipment required, adverse weather conditions can further restrict a researcher's ability to collect data anywhere and anytime. To mitigate this problem, we have developed a compact, multi-spectral automatic Aerial photographic system. This system's Multi-spectral camera is capable of the visible (RGB) and infrared (NIR) bands (3032*2008 pixel). It consists of a thermal infrared camera and automatic balance control, and can be managed by a palm-top computer. Other features includes a camera gimbal system, GPS receiver, weather sensor among others. We have evaluated the efficiency of this system in several field tests at the following locations: Kyongsang-bukdo beach, Nakdong river (at each site of mulkeum-namji and koryung-gumi), and Kyungahn River. Its tested ability in aerial photography, weather data, as well as GPS data acquisition demonstrates its flexibility as a tool for environmental data monitoring.

Real-time Parallel Processing Simulator for Modeling Portable Missile System and Performance Analysis (휴대용 유도탄 체계의 모델링과 성능분석을 위한 실시간 병렬처리 시뮬레이터)

  • Kim Byeong-Moon;Jung Soon-Key
    • Journal of the Korea Society of Computer and Information
    • /
    • v.11 no.4 s.42
    • /
    • pp.35-45
    • /
    • 2006
  • RIn this paper. we describe real-time parallel processing simulator developed for the use of performance analysis of rolling missiles. The real-time parallel processing simulator developed here consists of seeker emulator generating infrared image signal on aircraft, real-time computer, host computer, system unit, and actual equipments such as auto-pilot processor and seeker processor. Software is developed according to the design requirements of mathematic model, 6 degree-of-freedom module, aerodynamic module which are resided in real-time computer. and graphic user interface program resided in host computer. The real-time computer consists of six TI C-40 processors connected in parallel. The seeker emulator is designed by using analog circuits coupled with mechanical equipments. The system unit provides interface function to match impedance between the components and processes very small electrical signals. Also real launch unit of missiles is interfaced to simulator through system unit. In order to use the real-time parallel processing simulator developed here as a performance analysis equipment for rolling missiles, we perform verification test through experimental results in the field.

  • PDF

A Study of TCP LINK based Real-Time Secure Communication Research in the Ocean (해상에서 실시간 TCP 링크관절 보안통신 연구)

  • Yoo, Jaewon;Park, Dea-Woo
    • Proceedings of the Korean Institute of Information and Commucation Sciences Conference
    • /
    • 2014.05a
    • /
    • pp.250-253
    • /
    • 2014
  • Due to limited resource, marine communication is severely limited when compared to communications in land. Radio relay facilities, etc. based on a wired network through a long distance communication is possible. In addition, the aircraft is in the air, the ground-based network service based on long-range straight-line distance and elevation (LOS: Line of Sight) communications. On the other hand, the distance in a straight line to the sea, the sea level because communication is limited or through satellite, underwater communications relay equipment installed in the communication scheme has been investigated.. In this paper, using TCP-based real-time joint maritime security communication links were studied. Harsh marine environment, real-time communication that can provide secure communications and propose a LINK joint. In this study, more secure, and convenient communications at sea, a plan was presented to you.

  • PDF

The Modeling of Management Data and Drones Recommendation for Military Operation Support Mission (군 작전지원 임무 수행을 위한 드론 추천 및 관리 데이터 모델링)

  • Park, Keun-Seog;cheon, Sang-pil;Eom, Jung-ho
    • Convergence Security Journal
    • /
    • v.18 no.3
    • /
    • pp.133-140
    • /
    • 2018
  • As the core technology of the 4th Industrial Revolution is applied to drone, the potential for growth in the field of unmanned aerial vehicles is very large, and the utilization of civilian & military fields in the domestic & foreign is increasing rapidly. Because application areas of drone in the civilian field is various, it is excellent in terms of cost effectiveness and high value in utilization when it is used for military operation support mission. Especially, in the case of the Air Force, it is expected that military usage effectiveness will be high if drone replaces various air operations support missions such as aircraft inspection, supply of military supplies, base security. We find out the missions that can utilize drones for military operations support and propose the recommendation and data management plan accordingly. We recommend the most suitable drones and equipment that perform similar missions in the private sector and propose the data modeling of relational database.

  • PDF

Research of Small Gas Turbine Engine Control Logic by Engine Failure Mode Simulation (소형 가스터빈엔진 고장모드 모사를 통한 제어로직 연구)

  • Lee, Kyungjae;Kim, Sunguk;Back, Kyeungmi;Rhee, Dongho;Kang, Young Seok;Kho, Sunghee
    • Journal of the Korean Society of Propulsion Engineers
    • /
    • v.25 no.2
    • /
    • pp.88-97
    • /
    • 2021
  • The controller of the gas turbine engine is a component that needs to be developed for the development of the gas turbine engine because it is impossible to get the technology transferred from the engine manufacturer due to the import and export regulation. As a part of the engine control logic research, the Korea Aerospace Research Institute conducted a failure diagnostic research using a small gas turbine engine. Before simulating the engine fault, the ground test was performed to analyze normal behavior and performance of engine. Afterwards, the control logic analysis test equipment was established to simulate various engine fault. It is intended to provide background knowledge to engine control logic research for various engine failure conditions.

A Study of Certification of Lightning Indirect Effects on Cable Harness in Personal Air Vehicles (PAV 케이블 하네스에 대한 낙뢰 간접 영향성 인증 기법에 관한 연구)

  • Jo, Jae-Hyeon;Kim, Yun-Gon;Park, Se-Woong;Myong, Rho-Shin
    • Journal of the Korean Society for Aeronautical & Space Sciences
    • /
    • v.49 no.3
    • /
    • pp.251-262
    • /
    • 2021
  • The airworthiness certification of lightning indirect effects becomes an important issue in personal air vehicles (PAVs), which are being actively developed around the world. PAVs are very vulnerable to lightning strikes, because of miniaturization, use of the electric engines, composite materials, and application of unmanned navigation systems. In this study, we first examined various steps of certifications for lightning indirect effects shown in AC 20 136B issued by the Federal Aviation Administration (FAA). We then applied certification guidelines for equipment transient design level listed in RTCA DO 160G Section 22 to PAVs and investigated lightning transient environments inside the PAVs. We also analyzed the aircraft level tests specified in SAE ARP 5416A by using electromagnetic computational analysis software EMA3D. Finally, we analyzed the actual transient level for PAVs and derived the data necessary for conformity certification.

Design and Implementation of Integrated Production System for Large Aviation Parts (데이터 중심 통합생산시스템 설계 및 구현: 대형항공부품가공 사례)

  • Bae, Sungmoon;Bae, Hyojin;Hong, Kum Suk;Park, Chulsoon
    • Journal of Korean Society of Industrial and Systems Engineering
    • /
    • v.44 no.4
    • /
    • pp.208-219
    • /
    • 2021
  • In the era of the 4th industrial revolution driven by the convergence of ICT(information and communication technology) and manufacturing, research on smart factories is being actively conducted. In particular, the manufacturing industry prefers smart factories that autonomously connect and analyze data. For the efficient implementation of smart factories, it is essential to have an integrated production system that vertically integrates separately operated production equipment and heterogeneous S/W systems such as ERP, MES. In addition, it is necessary to double-verify production data by using automatic data collection technology so that the production process can be traced transparently. In this study, we want to show a case of data-centered integration of a large aircraft parts processing factory that requires high precision, takes a long time, and has the characteristics of processing large raw materials. For this, the components of the data-oriented integrated production system were identified and the connection structure between them was explained. And we would like to share the experience gained through the design and implementation case. The integrated production system proposed in this study integrates internal components based on data, which is expected to serve as a basis for SMEs to develop into an advanced stage, and traces materials with RFID technology.

Test Method and Results of Lightning Indirect Effects for Helicopter-mounted Missile System (헬기 탑재 유도탄 체계에 대한 낙뢰의 간접영향 시험방안 및 결과)

  • Lee, Jonghae;Lee, Sang-wook;Yang, Wonhyuk;Kim, Sangsik
    • Journal of the Korean Society for Aeronautical & Space Sciences
    • /
    • v.50 no.5
    • /
    • pp.359-365
    • /
    • 2022
  • Air-to-ground missile(AGM), which can be operated by being mounted on the outside of the aircraft, is capable of precision strikes, ensuring high survivability. Helicopter, which is one of the AGM operating platforms, is reported to experience a lightning strike once between 1000 and 20000 flight hours in average. When the lightning strikes the helicopter fuselage, lightning transient signal can be induced to internal and external electronic equipment cables through the skin of the helicopter. If the transient signal exceeding the criteria to electrically initiated device(EID) related to the explosive in the AGM can affect the safety of the helicopter by a warhead explosion, etc. In this paper, we suggest an indirect lightning test method to prove the safety of AGM on helicopter, and present the indirect lightning test results.

The Study on Optimal Placement and Systematic Performance Measurement Method for Communication/Navigation Antenna of Rotary Wing (회전익 항공기의 통신·항법 안테나 최적 위치설계를 통한 체계성능 측정방법 연구)

  • Sangwan No;Sangyoon Jin;Minsoo Kim;Howon Kang;Seungbeom Ahn
    • Journal of Aerospace System Engineering
    • /
    • v.17 no.4
    • /
    • pp.110-117
    • /
    • 2023
  • In this paper, the optimal placement of the rotary wing's communication and navigation antennas was evaluated by measuring their performance through ground simulations and flight tests. To select the mounting position of the communication and navigation antenna on the helicopter, after considering the shape and characteristics of the airframe, the radiation patterns, coupling analysis, equipment operation profiles, and antenna type analysis were performed for the aircraft-mounted antenna. Based on the analysis results, a procedure for sequentially performing voltage standing wave ratio (VSWR) measurement and antenna pattern test was established through ground and flight tests of the antenna. The systematic performance measurement method and procedure proposed in this paper were verified through ground and flight tests of the Light Armed Helicopter (LAH) system.