• Title/Summary/Keyword: Low-altitude

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A Study on Steady-state Performance Simulation of Smart UAV Propulsion System (신개념 비행체 추진시스템의 정상상태 성능모사 기법 연구)

  • 공창덕;강명철;기자영;양수석;이창호
    • Proceedings of the Korean Society of Propulsion Engineers Conference
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    • 2003.05a
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    • pp.177-182
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    • 2003
  • In this study, a performance model of the Smart UAV propulsion system with ducts, tip jets and variable main nozzle, which has flight capability of the rotary wing mode for the take-off/landing and low speed forward flight as welt as the fixed wing mode for high speed forward flight, has been newly developed. With the proposed model, steady-state performance analysis was performed at various flight modes and conditions, such as rotary wing mode, fixed wing mode, compound wing, mode altitude and flight speed. In investigation of performance analysis, it was noted that the operational capability of the propulsion system was limited due to the duct losses depending on each flight mode, and the limitation with the altitude variation case has much greater than that with the flight speed variation case.

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A Development of Instrumentation Radar Tracking Status Simulator (계측레이더 추적 시뮬레이터 개발)

  • Ye, Sung-Hyuck;Ryu, Chung-Ho;Hwang, Gyu-Hwan;Seo, Il-Hwan;Kim, Hyung-Sup
    • Journal of the Korea Institute of Military Science and Technology
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    • v.14 no.3
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    • pp.405-413
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    • 2011
  • Defense Systems Test Center in ADD supports increasingly various missile test requirements such as higher altitude event, multi target operation and low-altitude, high velocity target tracking. In this paper, we have proposed the development of instrumentation radar tracking status simulator based on virtual reality. This simulator can predict the tracking status and risk of failure using several modeling algorithms. It consists of target model, radar model, environment model and several algorithms includes the multipath interference effects. Simulation results show that the predict tracking status and signal are similar to the test results of the live flight test. This simulator predicts and analyze all of the status and critical parameters such as the optimal site location, servo response, optimal flight trajectory, LOS(Line of Sight). This simulator provides the mission plan with a powerful M&S tool to rehearse and analyze instrumentation tracking radar measurement plan for live flight test at DSTC(Defense Systems Test Center).

The introduction of Engine Performance Test for Miniature Turbojet Engine considering humidity effects (습도 영향을 고려한 초소형 터보제트 엔진 성능시험 소개)

  • Lee, Bo-Hwa;Lee, Kyung-Jae;Yang, Soo-Seok;Kim, Yu-Il
    • Proceedings of the Korean Society of Propulsion Engineers Conference
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    • 2010.11a
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    • pp.335-338
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    • 2010
  • The moisture in the atmosphere exerts a lot of influence upon Gas turbine engine performances. There is a noticeable influence of wet air at the summer sea level, high flight mach number and low engine rpm increasingly. An altitude Engine Test Facility is used to accomplish the engine performance tests at dry air condition and wet air condition, through which engine performance results is revealed. In the result, net thrust and specific fuel consumption measured -2.826% and 1.325%, respectively at wet air condition compared to dry air condition.

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A Study on Development of Small Sensor Observation System Based on IoT Using Drone (드론을 활용한 IoT기반의 소형센서 관측시스템 개발 가능성에 대한 소고)

  • Ahn, Yoseop;Moon, Jongsub;Kim, Baek-Jo;Lee, Woo-Kyun;Cha, Sungeun
    • Journal of Environmental Science International
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    • v.27 no.11
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    • pp.1155-1167
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    • 2018
  • We developed a small sensor observation system (SSOS) at a relatively low cost to observe the atmospheric boundary layer. The accuracy of the SSOS sensor was compared with that of the automatic weather system (AWS) and meteorological tower at the Korea Meteorological Administration (KMA). Comparisons between SSOS sensors and KMA sensors were carried out by dividing into ground and lower atmosphere. As a result of comparing the raw data of the SSOS sensor with the raw data of AWS and the observation tower by applying the root-mean-square-error to the error, the corresponding values were within the error tolerance range (KMA meteorological reference point: humidity ${\pm}5%$, atmospheric pressure ${\pm}0.5hPa$, temperature ${\pm}0.5^{\circ}C$. In the case of humidity, even if the altitude changed, it tends to be underestimated. In the case of temperature, when the altitude rose to 40 m above the ground, the value changed from underestimation to overestimation. However, it can be confirmed that the errors are within the KMA's permissible range after correction.

The Development of Mortar POLAR Program with Windward Wind Speed use Drones (드론을 활용한 풍향풍속이 적용된 박격포용 극표정법 프로그램 개발)

  • Hui Huang;Jung Hwan Kim
    • IEMEK Journal of Embedded Systems and Applications
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    • v.18 no.4
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    • pp.185-194
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    • 2023
  • Currently, drones are used in various fields such as transportation, agriculture and military. Especially, drones for military use are developed and utilized in many ways such as reconnaissance and bombing to minimize one's own damages. Nevertheless, they are developed as new weapons of modern types, so it is difficult to use them together with existing weapons. In this study, a drone program for effective bombing of mortar, which is often used in modern warfare, is developed. In mortar, a forward soldier comprehends the location of enemy for its distance and altitude, input them in data computer of launching angle, and applies the result value to cannon to launch. However, the existing method has low accuracy of bombing because observing shall be done within 1km from the target, and measuring accurate direction and velocity of the wind is difficult. Whereas, in the program of this study, the location of target, GPS, direction and velocity of the wind, and altitude are measured through drone. Each digit is used to calculate bombing specification for optimal bombing through the calculating formula of launching angle. In addition, when specifications are input in the program, the calculation is done automatically, so that it can be used in various mortars and shells. With the use of the program in this study, the location of enemy can be comprehended, and bombing specifications can be calculated quickly. It also enables the intensity of the wind to be applied for accurate bombing.

The Geomorphological Development of Marine Terraces UHS (upper higher surface) and HHS (high higher surface) around Yeondae-san, Gampo-Eup, Southeastern Coast of Korea (한국 남동해안 감포 연대산 지역 해안단구 상고위면과 고고위면 지형발달)

  • Hwang, Sangill;Yoon, Soon-Ock
    • Journal of The Geomorphological Association of Korea
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    • v.27 no.4
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    • pp.13-28
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    • 2020
  • In this study, the distribution and topographic development of marine terraces, UHS (Upper Higher Surface) and HHS (High Higher Surface) at Yeondae-san area, Gampo-eup were discussed. We critically examined on the substance of the Yeongdong-myeon (a low-lying erosion surface) in the east coast of Korea. In study area, UHS including UHS-246m, UHS-241m, UHS-235m, UHS-220m, UHS-210m and UHS-220 is found on the highest altitude among the marine terraces in Korea. The existence of UHS requires new interpretation on topographical surface like Yeongdong-myeon, which has been commonly accepted as a theory in the society of Korean Geography. Since UHS is distributed continuously ascending on the altitude of HHS, the period of formation should be understood in the same context. And UHS of paleo-shoreline 246m has been estimated to be formed about 1.5 million years ago.

Plant Community Structure by the Slope and Altitude of Tongdaesan Area in Odaesan National Park (오대산 국립공원 동대산지역의 사면. 해발고에 따른 식물군집구조)

  • Lee, Kyong-Jae;Cho, Woo;Hwang, Seo-Hyun;Yim, Kyong-Bin
    • Korean Journal of Environment and Ecology
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    • v.9 no.2
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    • pp.133-146
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    • 1996
  • This study was conducted to analyse plant community structure by the altityed and slope in Tongdaesan area, Odaesan National Park. Sixty-three plots(each plots size was 100m$^{2}$) were set up and PWINSPAN and DCA method were used for vegetational structure analysis. Division of community was cleared altitude than part of slope With increasing elevation the importance values of Quercus mongolica, Tilia amurensis increased, while those of Fraxinus mandshurica, Betula schmidtii, Cornus controversa decreased. Survey plots were divided into 6 groups by the TWINSPAN and DCA method. The divided groups are T. amurensis community(I), Q. mongolica community(II) of upper part of slope of east and west, Q. mongolica-T. amurensis community(III) of middle part of slope, Q. mongolica-F. mandshurica community(IV), Pinus densiflora-B. schmidtii-Carpinus laxiflora community(V) of low elevation of east, F. mandshurica-C. controversa community(VI)of low elevation of west. Also, vegetational change were showed slope of east and west in Tongdaesan except top area for the last twenty yeras.

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An Improvement of Efficiently Establishing Topographic Data for Small River using UAV (UAV를 이용한 소하천 지형자료 구축에 관한 효율성 제고)

  • Yeo, Han Jo;Choi, Seung Pil;Yeu, Yeon
    • Journal of Korean Society for Geospatial Information Science
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    • v.24 no.1
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    • pp.3-8
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    • 2016
  • Due to the recent technical development and the enhancement of image resolution, Unmanned Airborne Vehicles(UAVs) have been used for various fields. A low altitude UAV system takes advantage of taking riverbed imagery at small rivers as well as land surface imagery on the ground. The bathymetric data are generated from the low altitude UAV system. The accuracy of the data is analyzed along water depths, comparing GPS observations and a DSM generated from UAV images. It is found that the depth accuracy of the geospatial data below 50 cm depth of water satisfies the regulation(${\pm}10cm$ spatial accuracy) of bathymetric surveying. Therefore this research shows that the geospatial data generated from UAV images at shallow regions of rivers can be used for bathymetric surveying.

Construction of Korean Space Weather Prediction Center: Space radiation effect

  • Lee, Jae-Jin;Cho, Kyung-Suk;Hwang, Jung-A;Kwak, Young-Sil;Kim, Khan-Hyuk;Bong, Su-Chan;Kim, Yeon-Han;Park, Young-Deuk;Choi, Seong-Hwan
    • Bulletin of the Korean Space Science Society
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    • 2008.10a
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    • pp.33.3-34
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    • 2008
  • As an activity of building Korean Space Weather Prediction Center (KSWPC), we has studied of radiation effect on the spacecraft components. High energy charged particles trapped by geomagnetic field in the region named Van Allen Belt can move to low altitude along magnetic field and threaten even low altitude spacecraft. Space Radiation can cause equipment failures and on occasions can even destroy operations of satellites in orbit. Sun sensors aboard Science and Technology Satellite (STSAT-1) was designed to detect sun light with silicon solar cells which performance was degraded during satellite operation. In this study, we try to identify which particle contribute to the solar cell degradation with ground based radiation facilities. We measured the short circuit current after bombarding electrons and protons on the solar cells same as STSAT-1 sun sensors. Also we estimated particle flux on the STSAT-1 orbit with analyzing NOAA POES particle data. Our result clearly shows STSAT-1 solar cell degradation was caused by energetic protons which energy is about 700 keV to 1.5 MeV. Our result can be applied to estimate solar cell conditions of other satellites.

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Airborne Measurements of Ozone and Its Precursors over Yeosu-Gwangyang Industrial Areas in the Southern Coast of Korea

  • Kim, So-Young;Seo, Seok-Jun;Park, Hyun-Ju;Son, Jung-Seok;Park, Ji-Hoon;Kim, Jong-Choon
    • Asian Journal of Atmospheric Environment
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    • v.7 no.3
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    • pp.139-151
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    • 2013
  • The purpose of this study is to understand distributional characteristics in the atmospheric concentrations of $O_3$ and its precursors based on data taken at the southern Korean coast. The average $O_3$ concentration in the high altitude was found to range from 32.3 to 90.8 ppb with a maximum concentration of 132 ppb. The ambient $O_3$ concentration was high at altitudes of 1000 m and 500 m above the southern sea near Gwangyang Bay and an industrial area containing emission sources. The daily mean concentrations of $NO_y$ and CO were 6.7-24.2 ppb and 0.152-0.487 ppm, respectively. During the aerial measurement period, the highest mean concentration of $O_3$ was observed on June 1. The aerial measurement results showed that the maximum ozone concentration was observed to be 132 ppb in the high altitude the southernmost part of Yeosu. The measurement of vertical wind fields in the air indicated that $O_3$ formed in the southernmost part of Yeosu was transported by strong southwesterly winds to the northeast of Gwangyang Bay. This led to a ground $O_3$ concentration of over 100 ppb in Jinju, the northeastern part of Gwangyang Bay. On August 9, when the maximum $O_3$ concentration was 50 ppb, the measurement results showed that $O_3$ concentrations were relatively low compared to other days. In particular, low $NO_2$ and TVOC concentrations were observed, both of which serve to form $O_3$ in photochemical reactions.