• Title/Summary/Keyword: Missions

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A Selection of Path Planning Algorithm to Maximize Survivability for Unmanned Aerial Vehicle (무인 항공기 생존성 극대화를 위한 이동 경로 계획 알고리즘 선정)

  • Kim, Ki-Tae;Jeon, Geon-Wook
    • Journal of the Korea Safety Management & Science
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    • v.13 no.2
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    • pp.103-113
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    • 2011
  • This research is to select a path planning algorithm to maximize survivability for Unmanned Aerial Vehicle(UAV). An UAV is a powered pilotless aircraft, which is controlled remotely or autonomously. UAVs are currently employed in many military missions(surveillance, reconnaissance, communication relay, targeting, strike etc.) and a number of civilian applications(communication service, broadcast service, traffic control support, monitoring, measurement etc.). In this research, a mathematical programming model is suggested by using MRPP(Most Reliable Path Problem) and verified by using ILOG CPLEX. A path planning algorithm for UAV is selected by comparing of SPP(Shortest Path Problem) algorithms which transfer MRPP into SPP.

Analysis of landing site for lander and rover on Moon and Mars

  • Seo, Haingja;Kim, Eojin;Kim, Joo Hyeon;Lee, Joo Hee;Choi, Gihyuk;Sim, Eun-Sup
    • The Bulletin of The Korean Astronomical Society
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    • v.37 no.2
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    • pp.105.1-105.1
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    • 2012
  • Moon and Mars have been explored by landers and rovers. Apollo missions landed five times on Lunar surface, and various rovers, including Curiosity landed and explored Mars. The selection of landing site have to be considered engineering and scientific side: the landing site to be available to land stably? the obstacle is not around the rover such as rocks and pothole? the landing site is valuable with scientific? And then landing site have to be the place which is satisfied two objects. We search the information about landing sites of Moon and Mars, and compile the conditions of landing sites. We expect that these data are useful when the landing site of Moon or Mars for Korean mission is selected.

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A Study on Dispatch of Japanese Missions during Chosen Period , and their facilities (朝鮮時代의 日本使節과 諸施設에 관한 硏究)

  • 허만형
    • Journal of the Korean housing association
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    • v.7 no.1
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    • pp.25-35
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    • 1996
  • This study investigated the history of Japanese delegation and their route to Han-Yang(Seoul) and reception and all sorts of facilities to elucidate the characteristics of the reception for Japaneses delegates and all sorts of facilities in the period of Chosun dynasty. The results of the study are as follows; 1) In the early period of the Chosun dynasty, diplomatic facilities for Japanese delegates were established in Pusanpo(Pusan), Jepo, Yumpo and also delegates were invited to Han-Yang through the designated route. 2) Japanese from all areas of Japan have been correspond to Chosun, and many Buddhist monks were reside to draw up the diplomatic document. Also, temples were built in Janpanese style. 3) In case of visit of the most reverend priest of Japan(Wang-guk-sa), Ta-rae-i and Su-pe-re were performed at Yun-dae-chung and Kaek-sa in Pusan. 4) Because of establishing diplomatic facilities (We-Gwan) and other supporting facilities (Kwan-A), Pusan has developed as only one diplomatic city in the period of Chosun dynasty.

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A Study of Simulation Model for Effectiveness Analysis Simulation of Unmaned Underwater Vehicle for Mine Searching (기뢰 탐색 작전용 무인잠수정 효과도 분석 시뮬레이션을 위한 시뮬레이션 모델 연구)

  • Hwang, A-Rom;Kim, Moon-Hwan;Lee, Sim-Yong
    • Journal of the Korea Institute of Military Science and Technology
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    • v.15 no.4
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    • pp.410-416
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    • 2012
  • In recent years, unmanned underwater vehicles(UUVs) have emerged as viable technical solution for conducting underwater search, surveillance, and clearance operations in support of mine countermeasure missions(MCMs) because of her autonomy and long time endurance capability. It is necessary for UUV for MCM system design to define system specification from various configuration alternatives. This paper introduces a simulation model for mine countermeasure mission effectiveness analysis and presents some simulation results under various tide conditions for validation of the proposed simulation model.

Echelons Scale Identification Scheme of Surveillance and Reconnaissance Sensor Network (감시정찰 센서네트워크에서 제대규모 식별 기법)

  • Choi, Ji-Hye;Kwon, Tae-Wook
    • Journal of the Korea Institute of Military Science and Technology
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    • v.13 no.3
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    • pp.438-444
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    • 2010
  • Surveillance and reconnaissance sensor network system is an application system based on ubiquitous sensor network technology. This technique is to avoid accidental close combat, to minimize the consumption of limited military resources and personnel, and to provide battlefield situational awareness information for the unit's future combat missions. In this paper, we have proposed a echelons scale identification scheme based on information obtained from surveillance and reconnaissance sensor network system.

The Analysis of GOCI CDOM for Observation of Ocean Environment Change (해양환경변화관측을 위한 GOCI CDOM 자료 분석)

  • Jeong, Jong-Chul
    • Journal of Environmental Impact Assessment
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    • v.22 no.4
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    • pp.389-395
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    • 2013
  • Geostationary Ocean Color Imager(GOCI), the World's first spaceborne ocean color observation satellite operated in geostationary orbit, was successfully launched on May 2010. The main missions of GOCI is the coastal environment monitoring of GOCI in order to meet the necessity of long-term climate change monitoring and research. The GOCI have higher spatial resolution than MODIS, $500m{\times}500m$, and 8 spectral ocean color channels. GOCI have a capability for observation on the coastal environment change, GOCI perform the observation with 8 times a day. In this paper, we presented the more improved results for observation on the coastal environment change than MODIS ocean color sensor and detected the spatial difference of CDOM for monitoring coastal environment change.

Integrated Design of Rotary UAV Guidance and Control Systems Utilizing Sliding Mode Control Technique

  • Hong, You-Kyung;Kim, You-Dan
    • International Journal of Aeronautical and Space Sciences
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    • v.13 no.1
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    • pp.90-98
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    • 2012
  • In this paper, the Integrated Guidance and Control (IGC) law is proposed for the Rotary Unmanned Aerial Vehicle (RUAV). The objective of the IGC law is to consider the nonlinear dynamic characteristics of the RUAV and to design a guidance law which takes into consideration the nonlinear relationship between kinematics and dynamics. In order to control the RUAV system, sliding mode control scheme is adopted. As the RUAV is an under-actuated system, a slack variable approach is used to generate the available control inputs. Through the Lyapunov stability theorem, the stability of the proposed IGC law is proved. In order to verify the performance of the IGC law, numerical simulations are performed for waypoint tracking missions.

System Requirement Analysis of Passive Microwave Radiometer in Earth Observation Satellite (지구관측위성 수동형 마이크로파 라디오미터의 시스템 설계 요구 사항 분석 연구)

  • Ryu, Sang-Burm;Yong, Sang-Soon;Lee, Sang-Kon;Lee, Seung-Hoon
    • Journal of Satellite, Information and Communications
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    • v.7 no.2
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    • pp.87-96
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    • 2012
  • In this research, we describe recent technologies and system requirements of the passive microwave radiometer used in Earth observation satellites. And we classify types of microwave radiometer system for Earth observation satellites according to observation targets and ways to scan and discuss a design method. Also, requirements of passive radiometer for Earth observation missions in the latest practical examples used and developed are analyzed in this research.

Study on Safety and Reliability of ETOPS using Aircraft Operation Simulation

  • Nam, K.W.;Kim, C.Y.
    • Journal of the Korean Society for Aviation and Aeronautics
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    • v.4 no.1
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    • pp.7-24
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    • 1996
  • A methodology has been developed for predicting aircraft reliability incorporating both C.C.F.s(Common-Cause Failures), and phased missions. Failure behaviour of an aircraft, or it's systems are predicted. Both independent failures, and C.C.F.s, are modelled by the Markov process, and simulated using Monte Carlo sampling with the robust variance reduction method. Prediction of safety and reliability is made through discrete-event simulation of aircraft operations. A case study is described for investigating the safety and reliability of the propulsion system of two-, three- and four-engined aircraft. This is particularly important for the design of ETOPS(Extended Range of Two-Engined Aircraft Operations) and results are presented for the cases with, and without the effect of C.C.F.s.

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Wave height from satellite altimetry and its comparison with ECMWF product

  • Kim, Seung-Bum;Cotton, P.David
    • Proceedings of the KSRS Conference
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    • 2002.10a
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    • pp.337-340
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    • 2002
  • Monitoring of wave height is important primarily to reduce storm risks at sea and along the coast. Wave heights in recent years have increased 50% for the last 40 years, thus requiring intensive monitoring. Satellite altimetry offers a powerful tool for regular and extensive monitoring of the wave height. We extracted significant wave height (SWH) using several altimeter missions from 1987-1995 over the Northwest Pacific and compared with ECMWF reanalysis (ERA) products. For large wave heights > 2.5 m, the ERA wave heights are smaller than the altimetric ones, while for small wave heights the ERA wave heights are larger. Comparison in SWH between altimetric derivations and ERA model products shows the discrepancy of 0.46-0.21$\times$SWH(m).

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