• Title/Summary/Keyword: reusable space system

Search Result 14, Processing Time 0.017 seconds

State of the Art in the Development of Methane/Oxygen Liquid-bipropellant Rocket Engine (메탄/산소 이원액체추진제 로켓엔진 기술개발 동향)

  • Kim, Jeong Soo;Jung, Hun;Kim, Jong Hyun
    • Journal of the Korean Society of Propulsion Engineers
    • /
    • v.17 no.6
    • /
    • pp.120-130
    • /
    • 2013
  • A study was conducted for the performance characteristics of methane taking recently the limelight in the world as a next-generation propellant, with the survey for state of the art in the development of methane/oxygen rocket engine being accompanied. Liquid methane as a rocket fuel has the favorable characteristics such as non-toxic, low cost, regenerative cooling capability, and potential for in-situ resource utilization (ISRU). The combination of liquid methane and liquid oxygen also provides the excellent performance including high specific impulse and low system mass. For these reasons, many researches have been actively carried out on the methane/oxygen engine, nevertheless, its technology readiness level is not that high enough just yet. Therefore, it is judged that it is the time to mitigate the technical gap with the space technology of advanced countries through a swift onset of the development of methane rocket engine.

Vector Heuristic into Evolutionary Algorithms for Combinatorial Optimization Problems (진화 알고리즘에서의 벡터 휴리스틱을 이용한 조합 최적화 문제 해결에 관한 연구)

  • Ahn, Jong-Il;Jung, Kyung-Sook;Chung, Tae-Choong
    • The Transactions of the Korea Information Processing Society
    • /
    • v.4 no.6
    • /
    • pp.1550-1556
    • /
    • 1997
  • In this paper, we apply the evolutionary algorithm to the combinatorial optimization problem. Evolutionary algorithm useful for the optimization of the large space problem. This paper propose a method for the reuse of wastes of light water in atomic reactor system. These wastes contain several reusable elements, and they should be carefully selected and blended to satisfy requirements as an input material to the heavy water atomic reactor system. This problem belongs to an NP-hard like the 0/1 knapsack problem. Two evolutionary strategies are used as approximation algorithms in the highly constrained combinatorial optimization problem. One is the traditional strategy, using random operator with evaluation function, and the other is heuristic based search that uses the vector operator reducing between goal and current status. We also show the method which perform the feasible test and solution evaluation by using the vectored knowledge in problem domain. Finally, We compare the simulation results of using random operator and vector operator for such combinatorial optimization problems.

  • PDF

Development of UAV Flight Control Software using Model-Based Development(MBD) Technology (모델기반 개발기술을 적용한 무인항공기 비행제어 소프트웨어 개발)

  • Moon, Jung-Ho;Shin, Sung-Sik;Choi, Seung-Kie;Cho, Shin-Je;Rho, Eun-Jung
    • Journal of the Korean Society for Aeronautical & Space Sciences
    • /
    • v.38 no.12
    • /
    • pp.1217-1222
    • /
    • 2010
  • This paper describes the Model-Based Development(MBD) process behind the flight control software of a close-range unmanned aerial vehicle(KUS-9). An integrated development environment was created using a commercial tool(MATLAB $Simulink^{(R)}$), which was utilized to design models for linear/nonlinear simulation, flight control law, operational logic and HILS(Hardware In the Loop Simulation) system. Software requirements were validated through flight simulations and peer reviews during the design process, whereas the models were verified through the application of a DO-178B verification tool. The integrity of automatically generated C code was verified by using a separate S/W testing tool. The finished software product was embedded on two different types of hardware and real-time operating system(uC/OS-II, VxWorks) to perform HILS and flight tests. The key findings of this study are that MBD Technology enables the development of a reusable and an extensible software product and auto-code generation technology allows the production of a highly reliable flight control software under a compressed time schedule.

Separate Factor Caching Scheme for Mobile Web Service (모바일 웹 서비스를 위한 요소분할 캐싱 기법)

  • Sim, Kun-Jung;Kang, Eui-Sun;Kim, Jong-Keun;Ko, Hee-Ae;Lim, Young-Hwan
    • The KIPS Transactions:PartD
    • /
    • v.14D no.4 s.114
    • /
    • pp.447-458
    • /
    • 2007
  • The objective of this study is to provide faster mobile web service by improving performance of Contents Cache used for mobile web service in the existing Mobile Gate System. It was found that two elements existed in Mark-Up page transcoded by Contents Generator. One of the elements was dependent only on the requested DIDL page and Mark-Up type. The other was dependent on each of the requested DIDL page, Mark-Up type, size of mobile display 모바일 장치 to request service, type of images available and color depth count of the images available. The conventional Contents Cache saved the entire Mark-Up page to hold both of the two elements. This caused the problem where storage space was not effectively used because reusable elements were repetitively saved in cache memory domain due to change in one of the elements even though all the other elements were the same. As a result, a larger number of transcoded Mark-Up pages could not be saved in the same cache memory size. Therefore, in this study, Mark-Up pages transcoded by Contents Generator were divided into two elements and were separately saved. Also, in order to respond to the demand for replacing data in cache with new data, this study applied two algorithms of LFU and LRU. This study proposed the method to implement cache performance of faster speed by enabling to save more number of the transcoded Mark-Up pages in the same cache storage space.