• Journal of Astronomy and Space Sciences
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• 제27권3호
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• pp.253-262
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• 2010

The electrical power system (EPS) of Korean satellites in low-earth-orbit is designed to achieve energy balance based on a one-orbit mission scenario. This means that the battery has to be fully charged at the end of a one-orbit mission. To provide the maximum solar array (SA) power generation, the peak power tracking (PPT) method has been developed for a spacecraft power system. The PPT is operated by a software algorithm, which tracks the peak power of the SA and ensures the battery is fully charged in one orbit. The EPS should be designed to avoid the stress of electronics in order to handle the main bus power from the SA power. This paper summarizes the results of energy balance to achieve optimal power sizing and the actual trend analysis of EPS performance in orbit. It describes the results of required power for the satellite operation in the worst power conditions at the end-of-life, the methods and input data used in the energy balance, and the case study of energy balance analyses for the normal operation in orbit. Both 10:35 AM and 10:50 AM crossing times are considered, so the power performance in each case is analyzed with the satellite roll maneuver according to the payload operation concept. In addition, the data transmission to the Korea Ground Station during eclipse is investigated at the local-time-ascending-node of 11:00 AM to assess the greatest battery depth-of-discharge in normal operation.

• 인터넷정보학회논문지
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• 제15권5호
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• pp.1-7
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• 2014

무선센서 네트워크(WSNs)는 일반적으로 수많은 센서노드들이 배치되어 데이터를 전송하며, 불필요한 데이터 전송으로 인해 에너지 낭비를 초래한다. 기존의 연구들은 주로 에너지 소모문제를 해결하는데 집중되었다. 하지만 실시간으로 정보전송이 필요한 어플리케이션에 대해서는 지연 보장 역시 고려되어야 한다. 본 논문은 생체시스템을 모방하여 무선센서망에서 에너지의 소모와 연시간을 줄이기 위한 BISA(Bio-inspired Scheduling Algorithm)를 제안한다. BISA는 에너지 효율성이 높은 라우팅경로를 탐색하고 다중채널을 이용해 데이터 전송경로를 다중화함으로써 데이터 전송을 위한 에너지소모와 지연시간을 최소화한다. 실험결과를 통해 제안한 알고리즘의 기존방식 보다 적은 에너지를 사용하며 동시에 요구지연 시간을 보장함을 확인한다.

• 제어로봇시스템학회:학술대회논문집
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• 제어로봇시스템학회 1999년도 제14차 학술회의논문집
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• pp.33-36
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• 1999

The KOMPSAT, which is scheduled to be launched by Taurus launch vehicle in late November of 1999, will be in a sun-synchronous orbit with an altitude of 685km, eccentricity of 0.001, inclination of 98deg and local time of ascending node of 10:50 a.m. Electronics and Telecommunications Research Institute and Daewoo Heavy Industry had jointly developed a KOMPSAT Simulator as a component of the KOMPSAT Mission Control Element. The MCE had been delivered to Korea Aerospace Research Institute for the KOMPSAT ground operation. It is being used for training of KOMPSAT ground station personnel. Each of satellite subsystems and space environment were mathematically modeled in the simulator. To verify the overall function of KOMPSAT simulator, a Launch and Early Orbit Phase(LEOP) operation simulations have been performed. The simulator had been verified through various tests such as functional level test, subsystem test, interface test, system test, and acceptance test. In this paper, simulation results for LEOP operations to verify flight software adapted into simulator, satellite subsystem models and environment models are presented.

• 한국멀티미디어학회논문지
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• 제20권4호
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• pp.593-605
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• 2017

In applications which are covered wide range, it is possible that one or more number of Unmanned Aerial Vehicle(UAV) squadrons are used to perform a mission. In this case, it is most important to communicate seamlessly between the UAV squadrons. In this paper, we applied the modified OLSR(OSLR-Pds) which can prediction for state of the link for the communication in UAV squadron, and applied the modified AOMDV which can build multi-path for the communication between UAV Squadrons. The mobility of nodes are modeled using Gauss-Markov algorithm, and relative speed between nodes were calculated by derive equation of movement, and thereby we can predict link state for in a squadron and between squadrons. An experiment for comparing AODV, AOMDV and the proposed routing protocol was conducted by three factors such as packet delivery ratio, end to end delay, and routing overhead. In experiment result, we make sure that the proposed protocol performance are superior in these three factors. However, if the density of the nodes constituting FANET are too low, and if the moving speed of node is very slow, there is no difference to others protocols.

• 대한전기학회:학술대회논문집
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• 대한전기학회 2007년도 심포지엄 논문집 정보 및 제어부문
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• pp.351-352
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• 2007

The sensor networking technique as the radio network which does not have the base infrastructure network. The sensor nodes oneself automatic compose the network and simultaneously accomplish two roles of the router and data source. The sensor network is kind of Ad-hoc network is a possibility of seeing from point. sensor networking technique is restricted that limit of the memory and the battery back with the resources of the node. The sensor nodes overcomes the restriction of the resources it is in the process of researching the multi-hop routing technique which the sensor network divided cluster routing techniques which are researched. this paper proposed using beamforming antenna which has the directivity of the electric wave. the beamforming antenna from the Ad-hoc network using technique. the proposal is that raises the efficient of data trans mission from the sensor network and extends the lift time of the sensor network.

• 한국통신학회논문지
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• 제38C권4호
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• pp.378-386
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• 2013

본 논문은 N 통신노드들이 다중 안테나 비재생 릴레이국의 협력으로 서로 데이터를 교환하는 다중방향 릴레이 시스템을 제안한다. 기존의 단방향 릴레이를 적용한 다중방향 통신의 경우 2N 전송 단계가 필요하나 제안하는 다중방향 릴레이 시스템은 단일 다중접속 단계와 N-1 방송 단계로 구성된 총 N 전송 단계만 필요로 한다. 특히 효율적인 방송 단계 전송을 위해 통신노드들을 쌍을 짓고 쌍이 아닌 통신노드들에게 간섭을 주지 않는 새로운 릴레이 빔형성 행렬과 통신노드 자가간섭 소거기를 제안한다. 평균 합 전송률로 성능을 평가한 결과, 제안 기법이 기존 기법의 성능을 향상시키며 그 이득은 릴레이 노드 안테나 수와 통신노드 수가 비슷할 때 더 커짐을 볼 수 있다. 이러한 제안 기법은 여러 선박간의 정보를 공유할 필요가 있는 해양 통신 환경에서 통신 거리를 확장하는 데 효과적으로 적용할 수 있을 것으로 기대된다.

• Journal of Astronomy and Space Sciences
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• 제29권1호
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• pp.33-40
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• 2012

Triplet Ionospheric Observatory (TRIO) CubeSatforIon, Neutral, Electron MAgneticfields (CINEMA) is a CubeSat with the weight 3 kg that will be operated in the orbit conditions of about 800 km altitude and $90^{\circ}$ inclination angle, using the S-band and ultra-high frequency (UHF)-band communication frequencies. Regarding the communication antenna loaded on the satellite, the two patch antennas has the downlink function in the S-band, whereas the two whip antennas has the function to receive the command sent by the ground station to the satellite in the UHF-band. The uplink ground station that communicates through the UHF-band with the CINEMA satellite was established at Kyung Hee University. The system is mainly composed of a terminal node controller, a transceiver, and a helical antenna. The gain of the helical antenna established at the Kyung Hee University ground station was 9.8 dBi. The output of the transceiver was set to be 5 W (6.9 dB) for the communication test. Through the far-field test of the established system, it was verified that the Roman characters, figures and symbols were converted into packets and transmitted to the satellite receiver in the communication speed of 9,600 bps.

• Journal of Astronomy and Space Sciences
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• 제29권3호
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• pp.315-320
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• 2012

We developed a mass-memory chip by staking 1 Gbit double data rate 2 (DDR2) synchronous dynamic random access memory (SDRAM) memory core up to 4 Gbit storage for future satellite missions which require large storage for data collected during the mission execution. To investigate the resistance of the chip to the space radiation environment, we have performed heavy-ion-driven single event experiments using Heavy Ion Medical Accelerator in Chiba medium energy beam line. The radiation characteristics are presented for the DDR2 SDRAM (K4T1G164QE) fabricated in 56 nm technology. The statistical analyses and comparisons of the characteristics of chips fabricated with previous technologies are presented. The cross-section values for various single event categories were derived up to ~80 $MeVcm^2/mg$. Our comparison of the DDR2 SDRAM, which was fabricated in 56 nm technology node, with previous technologies, implies that the increased degree of integration causes the memory chip to become vulnerable to single-event functional interrupt, but resistant to single-event latch-up.

• Journal of Communications and Networks
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• 제11권6호
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• pp.599-606
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• 2009

For many mission-critical related wireless sensor network applications such as military and homeland security, user's access restriction is necessary to be enforced by access control mechanisms for different access rights. Public key-based access control schemes are more attractive than symmetric-key based approaches due to high scalability, low memory requirement, easy key-addition/revocation for a new node, and no key predistribution requirement. Although Wang et al. recently introduced a promising access control scheme based on elliptic curve cryptography (ECC), it is still burdensome for sensors and has several security limitations (it does not provide mutual authentication and is strictly vulnerable to denial-of-service (DoS) attacks). This paper presents an energy-efficient access control scheme based on ECC to overcome these problems and more importantly to provide dominant energy-efficiency. Through analysis and simulation based evaluations, we show that the proposed scheme overcomes the security problems and has far better energy-efficiency compared to current scheme proposed byWang et al.

• 전기전자학회논문지
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• 제19권3호
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• pp.357-365
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• 2015

최근 항공기, 자동차와 같은 시스템들은 크기, 무게, 전력 등의 문제로 기존 연합형(Federated) 구조에서 모듈형(Modular) 구조로 개발되는 추세이며, 단일 하드웨어에 파티션 개념을 적용하여 다수의 논리적 노드들을 운용할 수 있는 파티션 운영체제도 등장하고 있다. 분산 복구 블록은 실시간 시스템에 적용 가능한 소프트웨어 결함 허용 기법으로 다수의 물리적 노드들을 동기화 시켜 동작시킴으로써 실시간 절체가 가능하도록 하는 설계 기법이다. 분산 복구 블록은 노드들 간의 실시간 동기화를 필요로 하기 때문에 단일 코어 기반의 파티션 구조에는 적합하지 않으며, 적용을 위해서는 멀티코어를 기반으로 하고 또한 AMP(Asymmetric Multi-Processing) 방식을 이용한 파티션 구조에 적용되어야 한다. 본 논문에서는 멀티코어 기반 supervised-AMP 가상화 방식의 파티션 운영체제를 이용한 분산 복구 블록 설계 기법을 제안한다. 또한 제안된 설계 기법의 유용성을 보이기 위하여 항공기용 비행제어시스템 시뮬레이션을 이용한 사례 연구를 보인다.