• Title/Summary/Keyword: space vehicles

Search Result 708, Processing Time 0.029 seconds

Comparison of the Mission Performance of Korean GEO Launch Vehicles for Several Propulsion Options (시스템 구성에 따른 정지궤도 발사체의 임무성능 비교)

  • Hong, Mir;Yang, Seong-Min;Kim, Hye-Sung;Yoon, Youngbin;Choi, Jeong-Yeol
    • Journal of the Korean Society of Propulsion Engineers
    • /
    • v.21 no.2
    • /
    • pp.60-71
    • /
    • 2017
  • A trajectory analysis program is developed using a 3DOF trajectory model for the performance analysis of geostationary launch vehicles by system options. Launch trajectory and the performance of injection at GTO was estimated using this program for several propellant options, engine types, number of engines and the location of launch site. Results of the analysis presents that the possibility of mission accomplishment by several design options using domestic launch sites and the development direction of GEO launch vehicles.

Information Propagation Neural Networks for Real-time Recognition of Load Vehicles (도로 장애물의 실시간 인식을 위한 정보전파 신경회로망)

  • Kim, Jong-Man;Kim, Hyong-Suk;Kim, Sung-Joong;Sin, Dong-Yong
    • Proceedings of the KIEE Conference
    • /
    • 1999.07b
    • /
    • pp.546-549
    • /
    • 1999
  • For the safty driving of an automobile which is become individual requisites, a new Neural Network algorithm which recognized the load vehicles in real time is proposed. The proposed neural network technique is the real time computation method through the inter-node diffusion. In the network, a node corresponds to a state in the quantized input space. Each node is composed of a processing unit and fixed weights from its neighbor nodes as well as its input terminal. The most reliable algorithm derived for real time recognition of vehicles, is a dynamic programming based algorithm based on sequence matching techniques that would process the data as it arrives and could therefore provide continuously updated neighbor information estimates. Through several simulation experiments, real time reconstruction of the nonlinear image information is processed 1-D LIPN hardware has been composed and various experiments with static and dynamic signals have been implmented.

  • PDF

A Frame Collision Reduction Method for Safety Message Broadcasting in IEEE1609.4/IEEE802.11p based VANETs

  • Wang, Lei;Jing, Weiping
    • KSII Transactions on Internet and Information Systems (TIIS)
    • /
    • v.12 no.3
    • /
    • pp.1031-1046
    • /
    • 2018
  • Vehicular ad hoc network (VANET) is a dedicated network to connect vehicles without any centralized administration or infrastructure. The wireless access in vehicular environments (WAVE) protocol leveraging IEEE 1609/802.11p is widely implemented for VANETs. However, in congested traffic situation, the performance of the WAVE system degrades significantly due to serious collision, especially for safety related broadcast services on the control channel (CCH) interval due to the inherent drawback of its collision avoidance mechanisms called carrier sense multiple access with collision avoidance (CSMA/CA). In this paper, we propose a method that can decrease the number of frame collisions in CCH with a few modifications to the IEEE 802.11p protocol. In the paper, vehicles still employ CSMA/CA to compete for the channel access opportunity. However, by taking advantage of periodicity of synchronization interval, a two-state switching scheme introducing two new inter frame space (IFS) is proposed to reduce the number of competing vehicles substantially and as a result, the collision probability is significantly decreased. The simulation results demonstrate the superiority of the proposed method in packet collision rate.

Technology Trend of Propellant Tank Vent Relief Valve for Launch Vehicle (발사체용 추진제 탱크 벤트릴리프 밸브 기술 동향)

  • Koh, Hyeon-Seok
    • Current Industrial and Technological Trends in Aerospace
    • /
    • v.9 no.1
    • /
    • pp.130-138
    • /
    • 2011
  • A vent relief valve performs as a safety valve, which ensures ventilation of propellant tank during filling and protection from tank overpressure after filling. Because of the reliability and cost saving, the virtually same vent relief valve has been used on all US cryogenic liquid fueled launch vehicles. Some modification to the valve has been applied to satisfy the various mission requirements of launch vehicles. This paper reviews the main technology trends of the vent relief valve applied to the propellant feed system for launch vehicle with respect to design and manufacture. This paper also introduces the operating technology of vent relief valve applied for launch vehicles of advanced countries in space development.

  • PDF

Real-Time Neural Networks for Information Propagation of Load Vehicles in Remote (원격지 자동차의 정보 전송을 위한 실시간 신경망)

  • Kim, Jong-Man;Kim, Won-Sop;Sin, Dong-Yong;Kim, Hyong-Suk
    • Proceedings of the KIEE Conference
    • /
    • 2003.07d
    • /
    • pp.2130-2133
    • /
    • 2003
  • For real-time recognizing of the load vehicles a new Neural Network algorithm is proposed. The proposed neural network technique is the real time computation method through the inter-node diffusion. In the network, a node corresponds to a state in the quantized input space. Each node is composed of a Processing unit and fixed weights from its neighbor nodes as well as its input terminal. The most reliable algorithm derived for real time recognition of vehicles, is a dynamic programming based algorithm based on sequence matching techniques that would process the data as it arrives and could therefore provide continuously updated neighbor information estimates. Through severa simulation experiments, real time reconstruction nonlinear image information is Processed. 1-D hardware has been composed and various experi with static and dynamic signals have implemented.

  • PDF

Research on the Lubrication Characteristics of Driving Modules (구동 모듈 감속기 윤활 특성에 관한 연구)

  • Kim, EunKyum;Kim, HyunChan;Park, JunYoung
    • Tribology and Lubricants
    • /
    • v.38 no.2
    • /
    • pp.70-72
    • /
    • 2022
  • In this study, we report on a power system developed as a decelerator for a driving module in an electric vehicle. The system is to be mounted in a limited space. The research focus was on development of miniaturization, light weight, and high power density. In particular, we aimed to minimize the layout of existing external components as integrated or built-in, and to maximize the power density by applying optimal cooling technology to increased requirements for developing modular power systems applicable to various OEM models. South Korean automakers ranked fourth in global electric-vehicle sales in 2020, but domestic sales are relatively slow. Despite government's expansion in subsidies for eco-friendly cars, consumers are delaying purchases after 2021 considering the cost-effectiveness of electric vehicles. In major European markets, the demand for electric vehicles exceeded the demand for diesel cars, and sales of hybrid cars, which used to represent eco-friendly cars, are slowing down as Toyota, started selling electric vehicles. In this study, the internal lubrication characteristics of a decelerator installed in an electric vehicle were analyzed in terms of the deceleration time while driving. By selecting the proper oil and oil viscosity, it was confirmed that there is no problem in lubricating the bearings and gears of the decelerator.

TOWARD A NEXT GENERATION SOLAR CORONAGRAPH: DEVELOPMENT OF A COMPACT DIAGNOSTIC CORONAGRAPH FOR THE ISS

  • Cho, K.S.;Bong, S.C.;Choi, S.;Yang, H.;Kim, J.;Baek, J.H.;Park, J.;Lim, E.K.;Kim, R.S.;Kim, S.;Kim, Y.H.;Park, Y.D.;Clarke, S.W.;Davila, J.M.;Gopalswamy, N.;Nakariakov, V.M.;Li, B.;Pinto, R.F.
    • Journal of The Korean Astronomical Society
    • /
    • v.50 no.5
    • /
    • pp.139-149
    • /
    • 2017
  • The Korea Astronomy and Space Science Institute plans to develop a coronagraph in collaboration with National Aeronautics and Space Administration (NASA) and to install it on the International Space Station (ISS). The coronagraph is an externally occulted one-stage coronagraph with a field of view from 3 to 15 solar radii. The observation wavelength is approximately 400 nm, where strong Fraunhofer absorption lines from the photosphere experience thermal broadening and Doppler shift through scattering by coronal electrons. Photometric filter observations around this band enable the estimation of 2D electron temperature and electron velocity distribution in the corona. Together with a high time cadence (<12 min) of corona images used to determine the geometric and kinematic parameters of coronal mass ejections, the coronagraph will yield the spatial distribution of electron density by measuring the polarized brightness. For the purpose of technical demonstration, we intend to observe the total solar eclipse in August 2017 with the filter system and to perform a stratospheric balloon experiment in 2019 with the engineering model of the coronagraph. The coronagraph is planned to be installed on the ISS in 2021 for addressing a number of questions (e.g., coronal heating and solar wind acceleration) that are both fundamental and practically important in the physics of the solar corona and of the heliosphere.

New Technologies of Space Launch Vehicles including Electric-Pump Cycle Engine (전기펌프사이클 엔진 등 민간분야 우주발사체 신기술고찰)

  • Jeong, Seung-Min;Kim, Kui Soon;Oh, Sejong;Choi, Jeong-Yeol
    • Journal of the Korean Society for Aeronautical & Space Sciences
    • /
    • v.44 no.2
    • /
    • pp.139-155
    • /
    • 2016
  • Present paper introduces the recent advances in space launch vehicle technologies. A brief survey is given for the space development programs in civil sector with their business model and key technologies. Advances in key technologies were reviewed in detail with more emphasis on the electric pump cycle engine for low cost high performance small launch vehicle, Electron, under development by Rocketlab Ltd., since their contributions would give good lessons for rocket scientists.

AN EXTENSION OF A RELIABLE WAVELENGTH COVERAGE OF THE AKARI NG GRISM MODE

  • Baba, Shunsuke;Nakagawa, Takao;Isobe, Naoki;Shirahata, Mai;Ohyama, Youichi;Yano, Kenichi;Kochi, Chihiro
    • Publications of The Korean Astronomical Society
    • /
    • v.32 no.1
    • /
    • pp.45-47
    • /
    • 2017
  • The Infrared Camera onboard the AKARI satellite carried out spectroscopic observations with a grism mode named NG, whose wavelength coverage was $2.5-5.0{\mu}m$. We reinvestigate the current flux calibration for the NG grism mode, with which calculated flux density implausibly decreases at $4.9{\mu}m$ especially for red objects due to the second-order light contamination. We perform a new spectral response calibration using blue and red standard objects simultaneously. New response curves which contain both the first-and second-order light are able to separate each contribution consistently and useful for studies of red objects such as CO ro-vibrational absorption in active galactic nuclei.

Performance Analysis of a Precise Explicit Guidance Algorithm for Space Launch Vehicles (우주발사체의 정밀한 외연적 유도 알고리듬 성능 분석)

  • Song, Eun-Jung;Cho, Sang-Bum;Park, Chang-Su;Roh, Woong-Rae
    • Journal of the Korean Society for Aeronautical & Space Sciences
    • /
    • v.40 no.10
    • /
    • pp.853-861
    • /
    • 2012
  • This paper considers one of the explicit guidance algorithms, which has been proposed by Jaggers, to determine the closed-loop guidance algorithm for upper stages of a 3-staged space launch vehicle. Its commanded thrust vector is closer to the optimal solution when compared with that obtained by using the well-known Powered Explicit Guidance (PEG), which has been developed through the Space Shuttle program. Its performance is evaluated here by applying for guidance of the launcher during the second and third stages. Furthermore, to generate more precise guidance commands, it is attempted not to use the approximate formulas for the derivation of the original guidance law, and it is shown that performance is improved in comparison with the original.