• Aerospace Engineering and Technology
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• v.7 no.1
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• pp.194-201
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• 2008

The launch vehicle upper stage generally executes collision and contamination avoidance maneuver after the satellite separation. Through this maneuver the satellite safely settles in its orbit and the launch vehicle moves away from the satellite with minimum contamination. In this paper collision and contamination avoidance maneuvers by foreign launch vehicles are analyzed. Criteria for satellite contamination during the avoidance maneuver is given for KSLV-I upperstage.

• Journal of the Korean Society for Aeronautical & Space Sciences
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• v.39 no.11
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• pp.1033-1041
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• 2011

In this paper, a collision avoidance maneuver frequency for the KOMPSAT-2 and the KOMPSAT-5 is analyzed. For the statistical prediction of the avoidance maneuver frequency, mission orbits, responsive time, accepted collision probabilities, and positional uncertainties of primary and secondary objects are considered. In addition, the collision avoidance maneuver frequency of the KOMPSAT-2 is compared to the case that NORAD catalog during one year is used to calculate that of the KOMPSAT-2. As a result, the collision avoidance maneuver frequency is one per year on average and effective factors on the statistical prediction of the avoidance maneuver frequency are investigated. Efforts to improve its prediction accuracy are also discussed.

• The Bulletin of The Korean Astronomical Society
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• v.37 no.2
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• pp.161.1-161.1
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• 2012

지구 정지궤도는 위성통신, 지구관측 그리고 우주과학을 위해 매우 귀중하고 제한된 자원으로 인식된다. 이에 따라 Inter-Agency Space Debris Coordination Committee (IADC)에서는 정지궤도에서 수명이 종료되는 위성에 대해서 정지궤도에 영향을 미치지 않도록 더 높은 고도로 폐기기동을 수행하도록 권고하고 있다. 그렇지만 여러 가지 사정으로 정상적인 폐기기동을 수행하지 않은 위성들이 많이 있으며 이와 같은 위성들은 정지궤도에서 운영되고 있는 위성에 접근하여 충돌위험을 야기하고 있다. 우리나라의 정지궤도 통신해양기상위성인 천리안은 2010년 6월 26일에 발사되어 동경 128.2도에서 성공적으로 운영되고 있다. 지난 2년 동안 천리안 위성의 궤도구간에 우주물체가 접근하여 충돌위험이 발생한 사례가 3 건이 있었으며 그 중 한 건인 러시아의 라두가 1-7 위성이 접근한 2011년 2월 7일에는 천리안 위성의 회피기동을 수행하였다. 다른 두 가지 사례는 2011년 6월 19일 러시아의 COSMOS 2379의 접근과 2012년 4월 6일 러시아의 SL-12 R/B(2)의 접근이다. 본 논문에서는 정지궤도 위성을 운영하고 있을 때 다른 우주물체가 접근하여 충돌위험이 발생했을 때 어떤 과정을 거쳐서 회피기동을 수행해야 하는가에 대한 문제를 다루고자 한다. 정지궤도 위성과 우주물체와의 거리차이를 최대화할 수 있는 회피기동 시각을 찾아내고 최근접 시각에 있어서 반경방향, 진행방향, 그리고 수직방향에서의 거리차이를 분석한다.

• Journal of the Computational Structural Engineering Institute of Korea
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• v.30 no.6
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• pp.501-506
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• 2017

An infrared seeking missile does not emit any signal by itself as it is guided by passive heat signature from an aircraft. Therefore, it is difficult for the target aircraft to notice the existence of incoming missile, making it a serious threat. The usage of MAW(missile approach warning) that can notify the approaching infrared seeking missile is currently limited due to its high cost. Furthermore, effectiveness of MAW against infrared seeking missile is not available in open literature. Therefore, effect of evasive maneuver by MAW on the survivability of the aircraft is simulated to evaluate the benefit of the MAW in this research. The lethal range is used as a measure of aircraft survivability. An aircraft flying at an altitude of 5km with Mach 0.9 being tracked by air-launched AIM-9 infrared seeking missile is considered in this research. As a variable for the evasive maneuver, the MAW recognition distance of 5~7km and the G-force of 3~7G that limits maximum directional change of the aircraft are considered. Simulation results showed that the recognition of incoming missile by MAW and following evasive maneuver can reduce the lethal range considerably. Maximum reduction in lethal range is found to be 29.4%. Also, the MAW recognition distance have a greater importance than the aircraft maneuverability that is limited by structural limit of the aircraft.

• The Journal of Korean Institute of Communications and Information Sciences
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• v.41 no.5
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• pp.574-580
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• 2016

In this paper, we will introduce the system that can control multiple vehicles on the road through Single Board Computers and V2I (Vehicle-To-Infrastructure). Also, we will propose the group evasive maneuver decision algorithm, which plays a critical role in deciding whether the vehicles in the system have to conduct evasive maneuvers to avoid obstacles on the road. In order to test this system, we have utilized Wi-Fi and TCP/IP for establishing the communication between multiple vehicles and the relay server, and observed their driving states on the road with obstacles. During the experiments, we have discovered that our original decision algorithm possesses high failure rate when there is frequency interference in ISM (Industrial Scientific Medical) band. In order to reduce this failure rate, we have implemented the data transition detector. This paper will focus on how the use of data transition detector can affect the reliability of the system under the frequency interference of ISM band. If this technology is improved and applied in the field, we will effectively deal with such dangerous situations as multiple collision accidents through vehicle-to-vehicle communication or vehicle-to-infrastructure communication. Furthermore, this can be applied to the autonomous driving technologies. This can be used as the reference data for the development of the similar system.

• Journal of the Korea Society for Simulation
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• v.20 no.4
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• pp.1-11
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• 2011

In the development phase of a torpedo, the effectiveness analysis is carried out to predict the performance and to learn how to use the torpedo. In order to obtain reliable data, it is required to model the tactical situation closely to the actual one. Because the submarine is a target of a lightweight torpedo, the anti-torpedo countermeasures of a submarine such as evasive maneuvering and TACM (Torpedo Acoustic Counter Measure) should be modeled in detail. In this paper, the evasive maneuvering is modeled reflecting the movement characteristics of the submarine. Furthermore various TACMs such as a floating-type decoy, a self-propelled decoy and jammers are also modeled. Then, effectiveness of a lightweight torpedo is measured and analyzed using the simulation program which is developed through the above modeling procedure.

• Journal of Advanced Navigation Technology
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• v.16 no.2
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• pp.197-203
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• 2012

In this paper, study the substantial issues which occurs upon free flight environment by performing separation assurance under multiple conflict(over 3 Aircraft), recovery en route under the terms of time constrains and fixed way point after the conflict avoidance, correlations between conflict detection distance and separation assurance by utilizing Autonomous flight algorithm. Result of this experiment demonstrates that the extension of detection distance is advantageous to solution of separation assurance and enhancing of flight efficiency, choose to maneuver by applying time constrain terms and fixed way point according to the situation of conflict prediction in case of recovery maneuver after the conflict avoidance. And separation assurance can be solved by applying 2 degrees or more of bank angle. When choosing the optimal bank angle could be drastically improved flight efficiency.

• Annual Conference of KIPS
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• 2020.11a
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• pp.308-311
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• 2020

최근 드론 규제를 완화하겠다는 정부의 발표로 앞으로 여러 분야에서 드론이 상용화되어 이용될 것으로 예상되지만, 자율비행에 있어서 장애물을 회피하는 문제가 상용화의 걸림돌로 남아있다. 이에 본 논문에서는 GPS 기반으로 드론을 직접 제작하고, 초음파 센서를 활용하는 회피기동을 구현하여 비교적 저렴한 가격으로 자율비행 드론 시스템을 설계하여 앞으로 나오게 될 스마트 모빌리티 제품군들의 상용화에 기여할 수 있기를 기대한다.

• Aerospace Industry
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• s.105
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• pp.50-51
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• 2009

보스니아 내전 지역을 정찰비행 중이던 미 해군 F/A-18F 슈퍼 호넷을 향해 갑자기 지대공 미사일 공격이 가해진다. 조종사는 미사일의 추적을 뿌리치기 위해 모든 방어 장비를 총 동원해 회피 기동을 펼치지만 결국 적진 한 복판에서 격추되고 만다. 지난 2002년 1월 개봉한 영화 에너미 라인스(Behind Enemy Lines) 초반에 등장하는 장면이다. 영화에서 묘사된 것과 같이 미사일은 피아를 불문하고 가장 강력한 공격무기이자 가장 대응하기 까다로운 무기다.

• Journal of Space Technology and Applications
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• v.4 no.1
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• pp.62-73
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• 2024

This study analyzed the effectiveness of orbital change through attitude change in nano-satellites operating in low Earth orbit (LEO) without thrusters, focusing on collision avoidance maneuvers. The results revealed that changes in the satellite's cross-sectional area significantly impact its in-track direction, influenced by the aspect ratio of cross-sectional area change and mission altitude. Notably, satellites at lower altitudes demonstrated significant reduction in collision risks with a small amount of attitude change. Through this study, it is judged that the changing the cross-sectional area through attitude maneuver is a sufficiently suitable method in the operation of nano-satellites without thrusters, and is expected to contribute to improving the safety of satellite operations in the New Space era.