• 한국군사과학기술학회지
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• 제16권6호
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• pp.733-738
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• 2013

A guidance kit transforming a general purpose bomb into an air-to-surface gliding bomb was developed. This guidance kit consists of a flight kit and a tail kit. Flight kit contains deployable wing, GPS/INS integrated navigation system, guidance and control system. Also this guidance kit was designed to use neither electrical nor mechanical interface with aircraft, and to increase dramatically the survivabilities of pilot and aircraft with the high accuracy and the mid-range non-powered gliding capability.

• 전기학회논문지P
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• 제57권3호
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• pp.209-214
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• 2008

A precision guided kit is a GPS/INS guided range extension system to improve the accuracy and availability of existing dumb bombs. The PSD(power supply device) installed in the GPS guided kit supplies electrical power to all electrical loads in the kit. In this paper, design process and test results of the PSD have been presented. Additionally, the performance results of the PSD during actual ground and flight tests have been described.

• 항공우주기술
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• 제13권1호
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• pp.153-165
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• 2014

멀티로터 비행체는 헬리콥터와 같은 제자리 비행이 가능하면서 구조적으로 간단한 형태를 가지며 상대적으로 높은 추력을 가지는 장점으로 인해 다양한 분야에서 활용되고 있다. 최근 레저용으로 개발된 Parrot사의 AR.Drone은 사용자를 위한 내부 안정화 루프를 탑재하고 있기 때문에 초보자들도 쉽게 조정할 수 있으며, SDK(Software Development Kit)를 제공함으로서 멀티로터를 이용한 연구에 쉽게 활용할 수 있는 특징이 있다. 또한 크기가 상대적으로 작으면서 저가이기 때문에 군집비행에 적용되기 적합한 비행체이다. 이에 본 논문에서는 다수의 AR.Drone을 이용하여 실내 군집비행을 위한 제어기 개발과정에 대해서 소개하고자 한다.

• 한국항공우주학회지
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• 제41권4호
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• pp.314-318
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• 2013

국내 최초로 개발되는 공대지 유도키트에 대하여 미국의 MIL-HDBK 및 STANDARD를 준용한 시험을 성공적으로 수행하였다. 각종 지상시험을 통하여 유도키트의 작동 성능과 내구성을 검증하였으며, 유도키트를 일반목적폭탄에 장착한 활공탄으로 비행시험을 수행하여 중거리 활공비행성능 및 정확도가 매우 양호함을 확인하였다.

• 한국군사과학기술학회지
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• 제16권4호
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• pp.486-492
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• 2013

The pivoting composite wing is developed for the kit to be mounted on the external stores. The wing has a pivoting structure for the installation to an aircraft and high aspect ratio to increase lift drag ratio. The wing needs to be light and have sufficient strength and stiffness to satisfy structural design requirements. The wing is designed with carbon fiber composite and the structural parts are integrated to reduce cost to manufacture. In order to verify the structural performances, the design load analysis and flight load survey, the static analysis and test, the ground vibration test and flutter analysis are performed. It is shown that the wing has sufficient structural strength and stiffness to satisfy the structural design requirements.

• Journal of Astronomy and Space Sciences
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• 제35권4호
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• pp.295-308
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• 2018

In this study, orbit determination (OD) simulation for the Korea Pathfinder Lunar Orbiter (KPLO) was accomplished for investigation of the observational arc-length effect using a sequential estimation algorithm. A lunar polar orbit located at 100 km altitude and $90^{\circ}$ inclination was mainly considered for the KPLO mission operation phase. For measurement simulation and OD for KPLO, the Analytical Graphics Inc. Systems Tool Kit 11 and Orbit Determination Tool Kit 6 software were utilized. Three deep-space ground stations, including two deep space network (DSN) antennas and the Korea Deep Space Antenna, were configured for the OD simulation. To investigate the arc-length effect on OD, 60-hr, 48-hr, 24-hr, and 12-hr tracking data were prepared. Position uncertainty by error covariance and orbit overlap precision were used for OD performance evaluation. Additionally, orbit prediction (OP) accuracy was also assessed by the position difference between the estimated and true orbits. Finally, we concluded that the 48-hr-based OD strategy is suitable for effective flight dynamics operation of KPLO. This work suggests a useful guideline for the OD strategy of KPLO mission planning and operation during the nominal lunar orbits phase.

• 한국위성정보통신학회논문지
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• 제4권2호
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• pp.12-19
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• 2009

현대 정보전에서 테러 및 전쟁, 그리고 재난사고 등에 대한 자료 수집, 목표물 추적 등의 임무수행에 탁월한 능력을 보이고 있는 무인 시스템의 중요성이 점점 증대되는 추세이다. 본 논문에서는 Satellite Tool Kit(STK)를 사용하여 UAV의 임무수행에 대한 가상의 궤도 시나리오를 작성하고 레이다 센서를 활용하여 목표물을 식별하는 과정을 제시한다. 무인 시스템의 전체적인 동작은 STK를 이용하여 가상의 UAV 항로를 설정한 후, UAV에 탑재된 SAR센서를 이용하여 지형, 지물 및 목표물에 대한 스캔을 수행한다. 또한 스캔 센서를 합성개구레이다(Synthetic Aperture Radar : SAR)로 가상 구현하여 무인기탑재 레이더에서 수신한 반사 신호로부터 목표물에 대한 모델을 확립하기 위해서 레이다 원시데이터를 추출한다. 가상 시나리오에서 추출된 목표물의 점표적을 생성하기 위해 SAR 신호 처리를 수행하는 과정을 보이고 마지막으로 링크 버짓 설계 및 분석한다.

• Journal of Astronomy and Space Sciences
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• 제36권3호
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• pp.213-223
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• 2019

This paper analyzes delta-Vs to maintain an extremely low altitude on the Moon and investigates the possibilities of performing a CubeSat mission. To formulate the station-keeping (SK) problem at an extremely low altitude, current work has utilized real-flight performance proven software, the Systems Tool Kit Astrogator by Analytical Graphics Inc. With a high-fidelity force model, properties of SK maneuver delta-Vs to maintain an extremely low altitude are successfully derived with respect to different sets of reference orbits; of different altitudes as well as deadband limits. The effect of the degree and order selection of lunar gravitational harmonics on the overall SK maneuver strategy is also analyzed. Based on the derived SK maneuver delta-V costs, the possibilities of performing a CubeSat mission are analyzed with the expected mission lifetime by applying the current flight-proven miniaturized propulsion system performances. Moreover, the lunar surface coverage as well as the orbital characteristics of a candidate reference orbit are discussed. As a result, it is concluded that an approximately 15-kg class CubeSat could maintain an orbit (30-50 km reference altitude having ${\pm}10km$ deadband limits) around the Moon for 1-6 months and provide almost full coverage of the lunar surface.

• 환경생물
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• 제22권4호
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• pp.487-493
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• 2004

To investigate the antifungal activity related protein in pesticidal bacteria, a bacterial strain LTD was isolated from soil collected at Gimje in Jeonbuk province, Korea, and identified as Bacillus subtilis LTD based on a API50 CHB kit and 168 rDNA sequencing. It has an antifungal activity against 9 plant pathogenic fungi in a paper disc assay. The antifungal activity- deficient mutant, B. subtilis mLTD was induced at a 5 kGy dose of $^{60}Co$ gamma radiation. Using the two-dimensional electrophoresis and the matrix assisted laser desorption ionization time-of-flight mass spectrometry, the comparison analysis of proteins between the wild and mutant were performed. A major intracellular serine proteinase IspA (MW: 32.5 kDa), a NAD (P) H dehydrogenase (MW: 20.0 kDa), and a stage II sporulation protein AA, SpoIIAA (MW: 14.3kDa) were detected only in the B. subtilis LTD. These results suggested that the functions of these proteins found only in the B. subtilis LTD could. be closely related to the antifungal activity against plant pathogenic fungi.

• 산업경영시스템학회지
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• 제39권3호
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• pp.1-9
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• 2016

NSS (Navigation satellite system) provides the information for determining the position, velocity and time of users in real time using satellite-networking, and is classified into GNSS (Global NSS) and RNSS (Regional NSS). Although GNSS services for global users, the exactitude of provided information is dissatisfied with the degree required in modern systems such as unmanned system, autonomous navigation system for aircraft, ship and others, air-traffic control system. Especially, due to concern about the monopoly status of the countries operating it, some other countries have already considered establishing RNSS. The RNSS services for users within a specific area, however, it not only gives more precise information than those from GNSS, but also can be operated independently from the NSS of other countries. Thus, for Korean RNSS, this paper suggests the methodology to design the satellite constellation considering the regional features of Korean Peninsula. It intends to determine the orbits and the arrangement of navigation satellites for minimizing PDOP (Position dilution of precision). PGA (Parallel Genetic Algorithm) geared to solve this nonlinear optimization problem is proposed and STK (System tool kit) software is used for simulating their space flight. The PGA is composed of several GAs and iterates the process that they search the solution for a problem during the pre-specified generations, and then mutually exchange the superior solutions investigated by each GA. Numerical experiments were performed with increasing from four to seven satellites for Korean RNSS. When the RNSS was established by seven satellites, the time ratio that PDOP was measured to less than 5 (i.e. better than 'Good' level on the meaning of the PDOP value) was found to 94.3% and PDOP was always kept at 10 or less (i.e. better than 'Moderate' level).