• Proceedings of the Korea Information Processing Society Conference
• /
• 2024.05a
• /
• pp.617-618
• /
• 2024

본 논문에서 핵심적으로 연구할 내용은 기존 논문에서 소개된 BERT-base 모델의 경량화 버전인 DistilBERT 모델을 임베디드 시스템(Raspberry PI 5) 환경에 탑재 및 구현하는 것이다. 또한, 본 논문에서는 임베디드 시스템(Raspberry PI 5) 환경에 탑재한 DistilBERT 모델과 BERT-base 모델 간의 성능 비교를 수행하였다. 성능 평가에 사용한 데이터셋은 SQuAD(Standford Question Answering Dataset)로 질의응답 태스크에 대한 데이터셋이며, 성능 검증 지표로는 EM(Exact Match) Score와 F1 Score 그리고 추론시간을 사용하였다. 실험 결과를 통해 DistilBERT와 같은 경량화 모델이 임베디드 시스템(Raspberry PI 5)과 같은 환경에서 온 디바이스 AI(On-Device AI)로 잘 작동함을 증명하였다.

• Journal of the Korean Society for Aeronautical & Space Sciences
• /
• v.31 no.5
• /
• pp.124-133
• /
• 2003

We propose an application of the Object-Oriented design methodology to develop operational flight program(OFP) for stores management computer(SMC) which manages and controls stores inventory, stores activation, launch for missiles, and release of the conventional weapons. For the development of SMC, a military version of PowerPC 603e is used as a central processing unit board and VxWorks real-time operating system is used. The Tornado software development environment(SDE) and the programming language Ada95 are used for OFP development. We design three layerd in the OFP for the independency of the software modules. An avionics system computer(ASC) simulator and a test bench are developed for the SMC integration test and verification test. And the tests are rigorously and successfully conducted.

• Journal of the Korean Society for Aeronautical & Space Sciences
• /
• v.33 no.9
• /
• pp.104-112
• /
• 2005

This paper presents the technique to develop an operational flight program(OFP) of avionic system computer(ASC) which integrates the avionics control, navigation and fire control and provides informations for flight, navigation and weapon aiming missions. For the development of the OFP of ASC, two i960KB chips are used as central processing units board and standard computer interface library(SCIL) which is built in house is used. The Irvine compiler corporation(ICC) integrated development environment(IDE) and the programming language Ada95 are used for the OFP development. We designed the OFP to a computer software configuration item(CSCI) which consists of to three parts for independency of software modules. The OFP has been verified through a series of flight tests. The relevant tests also have been rigorously conducted on the OFP such as software integrated test, and ground functional test.

• Journal of the Institute of Electronics Engineers of Korea TC
• /
• v.45 no.10
• /
• pp.10-16
• /
• 2008

Generally, the satellite circling round in a low orbit goes through Van Allen belt connecting with the magnetic fold, in which electronic components are easily damaged and shortened by charged particles moving in a cycle between the South Pole and the North Pole. In particular, Single Event Upset(SEU) by radiation could cause electronic device on satellite to malfunction. Based on the idea mentioned above, this study considersabout SEU effect on the On-board Computer(OBC) of STSAT-1 in the space environment radiation, and shows algorithm to cope with SEUs. In this experiment, it also is shown that the repetitive memory read/write operation called memory wash is needed to prevent the accumulation of SEUs and the choice for the period of memory wash is examined. In conclusion, it is expected that this research not only contributes to understand low capacity of On-board Computer(OBC) on Low Earth Orbit satellite(LEOS) and SaTReC Technology satellite(STSAT) series, but also makes good use of each module development of Korea Multi-Purpose Satellite(COMPSAT) series.

• Journal of Satellite, Information and Communications
• /
• v.11 no.3
• /
• pp.92-99
• /
• 2016

AIS(Automatic Identification System) is an vessel traffic management system which exchanges vessel data with other nearby ships, AIS base stations using VHF band. A domestic AIS base station is located along coast lines or island. So it is difficult to collect vessel data from the ocean. To solve this problem, we adopted AIS payload on the low earth orbit satellite. The AIS payload on the satellite is interfaced with OBC(On-Board Computer) via UART and the FSW(Satellite Flight Software) manages it. The FSW have to receive AIS command from ground station and forward to AIS payload. Similarly FSW have to receive response, OBP, OGP data from AIS payload and it is downlink to the ground station. So in this paper we describe the FSW design & implementation for AIS payload.

• Proceedings of the Korea Information Processing Society Conference
• /
• 2005.11a
• /
• pp.1375-1378
• /
• 2005

향후 국내에서 개발되는 저궤도 관측위성의 고성능 탑재컴퓨터로 유럽에서 자체적으로 개발하여 위성용으로 활용하고 있는 MCM-ERC32 를 사용할 예정이다. MCM-ERC32 는 크게 32-비트 ERC32SC 프로세서와 프로세서의 기능을 보완하고 추가적인 기능들을 제공하기 위해 제작된 ASIC인 VASI(Very Advanced Sparc Interface), 그리고 메모리(SRAM, DRAM, EEPROM, etc.)로 구성되어 있다. 위성의 탑재소프트웨어를 설계 및 개발하는데 있어서 가장 기본적으로 요구되는 기능이 타이머이다. 탑재소프트웨어는 타이머를 통하여 태스크들의 관리와 스케쥴링 등을 수행하게 된다. 위성과 같이 높은 정확도가 요구되는 실시간 임베디드 시스템에서는 타이머의 구현이 매우 중요하다. ERC32SC 프로세서 자체에서도 RTC, GPT(General Purpose Timer), WDT(Watchdog Timer)와 같은 기본적인 타이머 기능을 제공하지만 VASI 에서도 클락과 사이클이라는 개념을 이용한 RTC 를 제공한다. 어느 타이머를 사용하는가는 전적으로 개발자의 선택이다. ERC32SC 프로세서에서 제공하는 타이머는 상용의 임베디드 시스템에서 제공하는 기능과 동일하다. 본 논문에서는 위성탑재소프트웨어 개발에 필요한 RTC 를 설계하기 위한 MCM-ERC32 에서 제공하는 VASI RTC 의 구조와 기능에 대하여 소개하고자 한다.

• The Optical Journal
• /
• s.157
• /
• pp.42-48
• /
• 2015

• Bulletin of the Korean Space Science Society
• /
• 2005.10a
• /
• pp.75-75
• /
• 2005

• Proceedings of the Korea Information Processing Society Conference
• /
• 2005.11a
• /
• pp.1421-1424
• /
• 2005

저궤도 위성인 다목적실용위성 2호의 컴퓨터 시스템은 3개 프로세서로 구성된 분산처리 구조이며 프로세서와 프로세서, 프로세서와 주변 장치들과의 통신은 MIL-STD-1553B 버스를 통해 이루어진다. 이들 3개 프로세서들 상에서 실행되는 탑재소프트웨어는 위성의 하드웨어 및 주변 입출력 장치들을 제어 및 관리한다. 그리고 위성의 결함을 관리하는 기능과 비상시에는 지상과의 연결 없이 위성을 자동제어 하는 기능들 또한 탑재소프트웨어에 구현되어져있다. 본 논문에서는 저궤도 위성인 다목적실용위성-2호의 임무를 수행하기 위한 탑재소프트웨어의 구성 및 기능, 개발과정과 개발환경을 소개한다.

• Journal of the Society of Naval Architects of Korea
• /
• v.38 no.1
• /
• pp.86-98
• /
• 2001

Due to the rapid growth of ship building industry and the increment of ship construction in Korea, several hundred thousand of lifting lugs per year, have been installed at the lifting positions of ship block and removed after finishing their function, therefore. appropriate design system for the strength check or the optimal design of each lug structure has been required in order to increase the capability of efficient design. In this study, the design system of D-type lifting lug structure which is most popular and useful in shipyards, was developed for the purpose of initial design of lug structure. Developed system layout and graphic user interface for this design system based on the $C^{++}$ language were explained step by step. Through the illustration of one example of D-type lug designs, the efficiency of this design system was proved. Therefore, more efficient performance of practical lug structural design will be expected on the windows of personal computer using this design system.