• 한국군사과학기술학회지
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• 제24권3호
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• pp.328-338
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• 2021

A study on common modular design based on open standards to reduce the life cycle cost of ground weapon system is underway. Since the ground weapon system includes major mission equipment such as fire control system, it is essential to apply the concept of fault tolerance through automatic reconfiguration and blocking unspecified equipment through connectivity control. However, it is difficult to generalize due to the difference in operating characteristics for each system. In this paper, we propose a plug-and-play framework, which includes plug-and-play architecture and mechanism. The proposed method can be used in common by the application of each component as it is divided into a common service layer. In addition, the proposed connectivity control and autonomous reconfiguration method facilitates reflection of operating characteristics for each system. We constructed a verification environment that can simulate ground weapon systems and components, and verified that the proposed framework works through scenario-based functional tests.

• Advances in aircraft and spacecraft science
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• 제9권3호
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• pp.195-215
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• 2022

The increasing interest in CubeSat platforms ant their capability of enlarging the frontier of possible missions impose technology improvements. Miniaturized electrical propulsion (EP) systems enable new mission for multi-unit CubeSats (6U+). While electric propulsion systems have achieved important level of knowledge at equipment level, the investigation of the mutual impact between EP system and CubeSat technology at system level can provide a decisive improvement for both the technologies. The interaction between CubeSat and EP system should be assessed in terms of electromagnetic emissions (both radiated and conducted), thermal gradients, high electrical power management, surface chemical deposition, and quick and reliable data exchanges. This paper shows how a versatile CubeSat Test Platform (CTP), together with standardized procedures and specialized facilities enable the acquisition fundamental and unprecedented information. Measurements can be taken both by specific ground support equipment placed inside the vacuum facility and by dedicated sensors and subsystems installed on the CTP, providing a completely new set of data never obtained before. CTP is constituted of a 6U primary structure hosting the EP system, representative CubeSat avionics and batteries. For the first test campaign, CTP hosts the ambipolar plasma propulsion system, called Regulus and developed by T4I. After the integration and the functional test in laboratory environment, CTP + Regulus performed a Test campaign in relevant environment in the vacuum chamber at CISAS, University of Padua. This paper is focused on the test campaign description and the main results achieved at different power levels for different duration of the firings.

• 우주기술과 응용
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• 제2권3호
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• pp.187-194
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• 2022

안테나의 고속 정밀 지향성 확보를 위해 동작되는 모터의 구동에 의한 외란의 크기는 극히 미소함에도 불구하고, 정밀 지향 성능이 요구되는 관측 위성의 영상 품질을 저해하는 주요 원인으로 작용하게 된다. 고해상도 관측위성의 지향 성능 향상을 통한 고해상도 영상정보 획득을 위해서는 지향성 안테나의 모터 구동시 발생하는 미소진동(Jitter)이 주요 임무 장비에 전달되지 않도록 적절한 진동절연 및 저감 설계가 요구된다. 본 논문에서는 실제 위성에 적용된 지향성 안테나 진동저감 장치에 대해 개발과정과 적용 전후의 미소 진동 저감 효과에 대해 살펴보고자 한다. 이 장치는 별다른 인터페이스 추가 장비 없이, 지향성 안테나 구동부 내에 있는 기어 하나만을 스프링 댐퍼 기어 형태로 교체함으로서, 발생되는 지터문제를 획기적으로 개선할 수 있는 방법으로 고안되었으며, 이 방식은 2015년에 발사된 서브미터급 고해상도 지구관측 위성에 처음으로 적용되어 발사되었으며, 현재까지 성공적으로 운용 중에 있다.

• 문화기술의 융합
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• 제10권4호
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• pp.589-594
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• 2024

본 연구는 LTE-Cat.M1 모듈을 사용하여 Sounding Rocket LTE 통신 시험 결과를 소개한다. 개발된 LTE 데이터 송수신 시스템은 임무탑재장비와 지상관측장비로 구성되며, 10 Hz의 속도로 일정하게 임무탑재장비로부터 데이터를 송신하여 지상관측장비에서 수신 시 계측되는 데이터 사이 시간을 바탕으로 지연율을 확보하였다. 실제 비행시험의 정확도를 높이기 위하여 지상 네트워크 지연율 시험과 하드웨어 내부 지연율 시험, 지상 시험을 수행하였다. 비행 시험 결과 상승 단계에서 핸드오버에 실패하여 13초간 통신이 유실되었음을 확인하였고, 이후 낙하산이 전개되어 일정한 위치 변위를 가진 상황에서 통신이 다시 연결됨을 확인하였다. 최종적으로 LTE-Cat.M1 기술은 Sounding Rocket 임무 중 하강 단계 관측 임무나 데이터 백업에 사용할 수 있을 것으로 기대한다.

• Advances in aircraft and spacecraft science
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• 제5권4호
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• pp.459-475
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• 2018

In the field of aerospace engineering, accurate control of a spacecraft's orientation is often very important to mission success. Therefore, attitude control is a technically plentiful and extensively studied subject in controls literature during recent decades. This investigation of spacecraft attitude control is assumed to address two important aspects of the problem solutions. One sliding mode anti-disturbance control for utilization of faulty actuator components and another one disturbance observer based control to improve the pointing accuracy in the absence of anti-vibration equipment for the elastic appendages like a solar panel. Simultaneous occurrence of vibration due to flexible appendages and reaction degradation due to failure in attitude actuators complicates this case. The advantage of this method is acquisition proper control by the combination of disturbance observer and sliding mode compensation that form a fault tolerant control for the concerned satellite attitude control system. Furthermore, the proposed composite method indicates that occurrence the failure in actuators and even elastic solar panel vibration effect may be handled directly without reconfiguring the control components or providing piezoelectric devices. It's noteworthy, attitude quaternion and angular velocity commands are robustly tracked via controllers to become inclined to zero.

• 전기학회논문지
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• 제57권3호
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• pp.403-408
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• 2008

The gyroscope is the sensor for detecting the rotation in inertial reference frame and constitute the navigation system together an accelerometer. As the inertial reference equipment for attitude determination and control in the satellite, the mechanical gyroscope has been used but it bring the disturbance for mass unbalance so the disturbance give a bad influence to the observation satellite mission because the mechanical gyroscope has the rotation parts. During the launch. The mechanical gyroscope is weak in vibration, shock and has the defect of narrow operating temperature range so it need the special design in integration. Recently the low orbit observation satellite for seeking the high pointing accuracy of image camera payload accept the FOG(Fiber Optic Gyro) or RLG(Ring Laser Gyro) for the attitude determination and control. The Ring Laser Gyro makes use of the Sanac effect within a resonant ring cavity of a He-Ne laser and has more accuracy than the other gyros. It need the 1000V DC to create the He-Ne plasma in discharge tube. In this paper, the design process of the High Voltage Power Supply for RLG(Ring Laser Gyroscope) is described. The specification for High Voltage Power Supply (HVPS) is proposed. Also, The analysis of flyback converter topology is explained. The Design for the HVPS is composed of the inverter circuit, feedback control circuit, high frequency switching transformer design and voltage doubler circuit.

• 항공우주기술
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• 제9권2호
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• pp.80-89
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• 2010

트랜스폰더는 지상국과 위성 사이의 텔레메트리와 텔레커맨드 운영을 위한 주요한 장비이다. 최근 트랜스폰더는 통신 방식과 사용자의 요구 사항에 따라 단순 표준화된 트랜스폰더와 데이터 릴레이 위성을 위한 소규모 사용자 트랜스폰더, 대규모 사용자를 위한 이중 모드 트랜스폰더 및 심우주 미션을 위한 심우주 트랜스폰더 등의 다양한 트랜스폰더가 개발되어 왔다. 특히 디지털 기술을 근간으로 하는 디지털 트랜스폰더 기술이 위성 통신 분야에서 주목 받고 있다. 본 논문은 다양한 트랜스폰더 기술과 기존의 아날로그 트랜스폰더 기술에 접목된 최신 기술인 디지털 트랜스폰더에 대하여 기술하였다.

• 한국항공운항학회지
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• 제22권1호
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• pp.22-31
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• 2014

Military UAV(Unmanned Aerial Vehicle) operated as a RC(Remotely Control) model level within the limit of the military special use airspace until now. However, the high and medium altitude of URA(Unmanned Reconnaissance Aircraft) which the ROKAF have been trying to import recently is at the UAV level and needs the criteria for the classified airspace flights. The required flight criteria includes operator location, mission operation limit, equipment, etc., which are the principle and standard applied based on the airspace use for UAV. Also, the general flight rules, visual flight rules, instrument flight rules are required in order to have to be applied to the actual flight. Besides, an appliance regulation needs to be arranged regarding two-way communication, ATC and communication issue, airspace and area in-flight between UAS( Unmanned Aircraft System) users. An operation of the UAV in the air significantly requires the guarantee of the aircraft's capacity, and also the standardized flight criteria. A safe and smooth use is ensured only if this criteria is applied and understood by the entire airspace users. For the purpose, a standardized military UAV flight operations criteria that is to be applied for each airspace by UAV is to be prepared through analysis of the present state, a legend UAV system, and a special character analysis.

• 품질경영학회지
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• 제21권2호
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• pp.1-16
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• 1993

Early generations of products had little to no inherent capability to test themselves. The technologies involved often required only visual inspection and limited probing to troubleshoot the system once it was turned over to maintenance personnel. However, as the complexity of military and commercial systems grew, symptoms of failure became less noticeable to the operator. Therefore, the procedure to access, inspect, repair and replace a component became complicated, the requirements for personnel skill and testing equipment increased. and it took too long of a time to maintain a system. Meanwhile, the need for availability became more mission-critical and maintenance become very expensive. The obvious solution was to design in-system circuits or devices to self-test the primary system, the Built-In-Test(BIT) was born. This approach has continued right on up through present systems and is an integral part of systems now being designed. The object of this paper is to present a state-of-the-art research for filtering out the BIT diagnosis mistakes using Bayesian analysis and develop the algorithm for Redundant systems with BIT to improve BIT diagnosis.

• 한국도서관정보학회지
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• 제40권4호
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• pp.177-198
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• 2009

국내 도서관은 정보화 시대에 적응하기 위하여 이용자에게 컴퓨터 사용환경을 일찍부터 제공하였다. 하지만 오늘날은 컴퓨터 사용환경이 일반화되어 전자정보실에 대한 변화가 필요한 시점이다. 이에 문헌정보학과 학생 78명으로 하여금 직접 전자정보실을 이용해 보게 하여 이용에 편리한 점과 불편했던 점을 기술하게 하였다. 이용사례 결과를 분석하여 전자정보실의 바람직한 변화 방향을 찾고자 하였다. 그 결과 사서에 의해 제공되는 정보서비스에서 불만이 가장 많았고, 그 이외에 시설과 장비 그리고 공간 순으로 많았다. 이를 개선하기 위한 방안으로는 도서관에서 전자정보실의 기능을 명확히 하는 미션과 서비스 방향을 정확히 제시하여야 하고, 사서는 전자정보실이 디지털 자료와 아날로그 자료 그리고 정보통신 기술지원이 동시에 제공되는 현대화된 레퍼런스 룸으로 인식해야 할 것이다.