• Title/Summary/Keyword: mission control system

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A Short Course Development and Analysis to Recognize Importance of Software for Youth using Arduino and App Inventor

  • Shim, Jooeun;Ko, Jooyoung;Shim, Jaechang
    • Journal of Multimedia Information System
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    • v.2 no.1
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    • pp.187-192
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    • 2015
  • The aim of this study was to develop and analyze a short course educating App Inventor and Arduino that showed the importance of software for youth. The course consists of a total of 10 missions for a 4 hour course divided into 2 parts, each 2 hours respectively. We conducted a basic course of Arduino for hardware and software, Processing for server programming, and App Inventor for programming for smartphones. The final mission was to send a signal to a server with a smartphone and to control light connected to a relay which passes Arduino connected with a server and serial communication. Participants completed 95% of missions, and we found the course had an educational effect for improving creativity and realization of software importance.

A Study on Licence Management Model for Contents Circulation which Ubiquitous Environment is Safe (유비쿼터스 환경의 안전한 콘텐츠 유통을 위한 라이센스 관리 모델 연구)

  • Cho, Hyun-Seob;Oh, Myoung-Kwan
    • Proceedings of the KAIS Fall Conference
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    • 2011.05a
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    • pp.366-370
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    • 2011
  • This paper propose an interested digital rights protection scheme using license agent to address problems facing contemporary DRM approached : static digital rights management, and limited application to on-line environment. We introduce a dynamic mission control technology to realize dynamic digital rights management. And we incorporate license agent to on- and off-line monitoring and tracking. The proposed system prevent illegal access and use by using PKI security method, real time action monitoring for user, data security for itself.

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DEVS-based Digital Twin Simulation Environment Modeling for Alternative Route Selection in Emergency Situations of Unnamed Aerial Vehicles (무인비행체의 유사시 대안 경로 선택을 위한 DEVS 기반 디지털 트윈 시뮬레이션 환경 모델링)

  • Kwon, Bo Seung;Jung, Sang Won;Noh, Young Dan;Lee, Jong Sik;Han, Young Shin
    • Journal of Korea Multimedia Society
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    • v.25 no.8
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    • pp.1007-1021
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    • 2022
  • Autonomous driving of unmanned aerial vehicles may have to pay expensive cost to create and switch new routes if unexpected obstacles exist or local map updates occured by the control system due to incorrect route information. Integrating digital twins into the path-following process requires more computing resources to quickly switch the wrong path to an alternative path, but it can quickly update the path during flight. In this study, we design a DEVS-based simulation environment which can modify optimized paths through short-term simulation of multi-virtual UAVs for applying digital twin concepts to path follow. Through simulation, we confirmed the possibility of increasing the mission stability of UAV.

Development of the TVC Battery for High Voltage Loads in KSLV-I Upper Stage (KSLV-I 상단부 고전압 부하용 TVC 배터리 개발)

  • Kim, Myung-Hwan;Ma, Keun-Sum;Lim, You-Chol;Lee, Jae-Deuk
    • Aerospace Engineering and Technology
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    • v.7 no.2
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    • pp.110-116
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    • 2008
  • This paper gives a brief summary of the TVC battery design description, specifications and test results. The TVC battery for KSLV-I upper stage contains 168 Sony l8650VT high power lithium-ion cells. It configured as 2 strings in parallel, with each string containing 84 series connected cells. This allows to meet nominal 270V voltage and capacity requirements specified for the mission of the Thrust Vector Control(TVC) system. The loads profile of the TVC system has short duration, high current pulse. To power such a system with minimal mass, the battery employed l8650VT Cells. This cell is specifically designed for high rate applications and is capable of a 10C continuous discharge.

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A Proposal on the Aviation Rules of the Military UAV in the National Airspace System (국가공역체계 내에서 군용 무인항공기 비행규칙에 관한 제언)

  • Park, Wontae;Lee, Kangseok;Im, Kwanghyun
    • Journal of the Korean Society for Aviation and Aeronautics
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    • v.22 no.1
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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.

DEVELOPMENT OF MISSION ADN SPACECRAFT DYNAMICS ANALYSIS SYSTEM FOR GEOSTATION COMMUNICATION SATELLITE (통신위성의 임무 및 위성체 동역학 해석 시스템 개발)

  • 공현철;김방엽;김정아;윤진원
    • Journal of Astronomy and Space Sciences
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    • v.15 no.1
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    • pp.251-260
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    • 1998
  • We consider the motion of the subsystems as separate bodies as well as the entire satellite for the attitude and orbit control of a communication satellite by multi-body modeling technique. Thus, the system, can be applied to a general communication satellite as well as a specific communication satellite, i. e. Koreasat I,II. The simulation results can be viewed by two-dimensional graphics and three-dimensional animation. The graphical user interface(GUI) makes its usage much simpler. We have simulated a couple of scenarios for Koreasat I,II which are being operated as geostationary communication satellites to verify the system performance.

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Analysis of the Detection Time of Distress Signal for LEOSAR and MEOSAR Systems (LEOSAR 및 MEOSAR 시스템의 조난신호 탐지시간 해석)

  • Lim, Sang-Seok
    • Journal of Advanced Navigation Technology
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    • v.10 no.4
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    • pp.377-384
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    • 2006
  • In this paper the detection time of the distress signal for the satellite-based search and rescue (SAR) system is evaluated. Present LEOSAR system in operation employs a few Low-altitude Earth Orbit (LEO) satellites and hence provides poor and local coverage availability. This results in a considerably long waiting time for a distress beacon to be detected by a rescue mission control center. One can expect that the detection time of the distress signal will be significantly reduced if the proposed MEOSAR system, which is based on the Medium-altitude Earth Orbit (MEO) satellites, is implemented. Taking into account the influence of the obstacles on the beacon signal, simulations are carried out to evaluate the detection time of distress signals for the LEOSAR and MEOSAR systems and the corresponding results are analyzed.

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TWR based Cooperative Localization of Multiple Mobile Robots for Search and Rescue Application (재난 구조용 다중 로봇을 위한 GNSS 음영지역에서의 TWR 기반 협업 측위 기술)

  • Lee, Chang-Eun;Sung, Tae-Kyung
    • The Journal of Korea Robotics Society
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    • v.11 no.3
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    • pp.127-132
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    • 2016
  • For a practical mobile robot team such as carrying out a search and rescue mission in a disaster area, the localization have to be guaranteed even in an environment where the network infrastructure is destroyed or a global positioning system (GPS) is unavailable. The proposed architecture supports localizing robots seamlessly by finding their relative locations while moving from a global outdoor environment to a local indoor position. The proposed schemes use a cooperative positioning system (CPS) based on the two-way ranging (TWR) technique. In the proposed TWR-based CPS, each non-localized mobile robot act as tag, and finds its position using bilateral range measurements of all localized mobile robots. The localized mobile robots act as anchors, and support the localization of mobile robots in the GPS-shadow region such as an indoor environment. As a tag localizes its position with anchors, the position error of the anchor propagates to the tag, and the position error of the tag accumulates the position errors of the anchor. To minimize the effect of error propagation, this paper suggests the new scheme of full-mesh based CPS for improving the position accuracy. The proposed schemes assuring localization were validated through experiment results.

Comparison study of CPU processing load by I/O processing method through use case analysis (유즈케이스를 통해 분석해 본 I/O 처리방식에 따르는 CPU처리 부하 비교연구)

  • Kim, JaeYoung
    • Journal of Aerospace System Engineering
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    • v.13 no.5
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    • pp.57-64
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    • 2019
  • Recently, avionics systems are being developed as integrated modular architecture applying the modular integration design of the functional unit to reduce maintenance costs and increase operating performance. Additionally, a partitioning operating system based on virtualization technology was used to process various mission control functions. In virtualization technology, the CPU processing load distribution is a key consideration. Especially, the uncertainty of the I/O processing time is a risk factor in the design of reliable avionics systems. In this paper, we examine the influence of the I/O processing method by comparing and analyzing the CPU processing load by the I/O processing method through use of case analysis and applying it to the example of spatial-temporal partitioning.

A Development of the Operational Architecture of a Low Altitude Air Defense Automation System (저고도 방공자동화체계의 운용아키덱처 개발)

  • Son, Hyun-Sik;Kwon, Yong-Soo
    • Journal of the military operations research society of Korea
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    • v.34 no.1
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    • pp.31-45
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    • 2008
  • This paper describes a development of the operational architecture of a low altitude air defense automation system using a systems engineering approach. The future battlefield is changing to new system of systems that command and control by the network based BM/C4I. Also, it is composed of various sensors and shooters in an single theater. Future threats may be characterized as unmanned mewing bodies that the strategic effect is great such as UAVs, cruise missiles or tactical ballistic missiles. New threats such as low altitude stealth cruise missiles may also appear. The implementation of a low altitude air defense against these future threats is required to complex and integrated approach based on systems engineering. In this view, this work established an operational scenario and derived operational requirements by identifying mission and future operational environments. It is presented the operational architecture of the low altitude air defense automation system by using the CORE 5.0.