• Title/Summary/Keyword: Mission Planning System

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A Graphical User Interface Design for Surveillance and Security Robot (감시경계 로봇의 그래픽 사용자 인터페이스 설계)

  • Choi, Duck-Kyu;Lee, Chun-Woo;Lee, Choonjoo
    • The Journal of Korea Robotics Society
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    • v.10 no.1
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    • pp.24-32
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    • 2015
  • This paper introduces a graphical user interface design that is aimed to apply to the surveillance and security robot, which is the pilot program for the army unmanned light combat vehicle. It is essential to consider the activities of robot users under the changing security environment in order to design the efficient graphical user interface between user and robot to accomplish the designated mission. The proposed design approach firstly identifies the user activities to accomplish the mission in the standardized scenarios of military surveillance and security operation and then develops the hierarchy of the interface elements that are required to execute the tasks in the surveillance and security scenarios. The developed graphical user interface includes input control component, navigation component, information display component, and accordion and verified by the potential users from the various skilled levels with the military background. The assessment said that the newly developed user interface includes all the critical elements to execute the mission and is simpler and more intuitive compared to the legacy interface design that was more focused on the technical and functional information and informative to the system developing engineers rather than field users.

A Study on an Operational Availability Computation Model for Weapon Systems (무기체계 운용가용도 산정 모델에 관한 연구)

  • Kim, Hye-Lyeong;Baek, Soon-Heum;Choi, Sang-Yeong
    • Journal of the military operations research society of Korea
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    • v.35 no.3
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    • pp.17-30
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    • 2009
  • In this study, we propose the operational availability computation model that can be used on the weapon system's requirement planning phase. The proposed model consists of the time parameters of Ao(Operational Availability) for a system and each time parameter's estimation method. The time parameters for Ao computation are TT(Total Time) and TDT(Total Down Time). The time parameters are defined by considering OMS/MP(Operational Mode Summary/Mission Profile) elements. TT is a calendar time as a specific mission time at wartime or one year at peacetime. TDT consists of TPM(Total Preventive Maintenance time), TCM (Total Corrective maintenance time), TALDT(Total Administrative and Logistics Down Time). Then the estimation method for these time parameters are presented by the weapon systems types.

Distributed Task Assignment Algorithm for SEAD Mission of Heterogeneous UAVs Based on CBBA Algorithm (CBBA 기반 SEAD 임무를 위한 이종무인기의 분산형 임무할당 알고리듬 연구)

  • Lee, Chang-Hun;Moon, Gun-Hee;Yoo, Dong-Wan;Tahk, Min-Jea;Lee, In-Seok
    • Journal of the Korean Society for Aeronautical & Space Sciences
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    • v.40 no.11
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    • pp.988-996
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    • 2012
  • This paper presents a distributed task assignment algorithm for the suppression of enemy air defense (SEAD) mission of heterogeneous UAVs, based on the consensus-based bundle algorithm (CBBA). SEAD mission can be modeled as a task assignment problem of multiple UAVs performing multiple air defense targets, and UAVs performing SEAD mission consist of the weasel for destruction of enemy's air defense system and the striker for the battle damage assessment (BDA) or other tasks. In this paper, a distributed task assignment algorithm considering path-planning in presence of terrain obstacle is developed for heterogeneous UAVs, and then it is applied to SEAD mission. Through numerical simulations the performance and the applicability of the proposed method are tested.

Empirical Capability Assessment Methodology of Quick Look using Weapon Score of Joint Integrated Contingency Model (전구급 워게임 모형의 무기점수를 활용한 Quick Look의 실증적 능력평가 방법론)

  • Kim, Hyungkwon;Kim, Youngho
    • Journal of the Korea Society for Simulation
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    • v.26 no.1
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    • pp.55-67
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    • 2017
  • The requirement planning system of Korea military has used top down planning approach after introducing Joint Combat Development System since 2007. But this new system has not been propelled harmoniously because it does not have any connection with the current planning system. Due to current time-exhaustive analysis and assessment process in requirement planning system, it not only delays proper decision making, but also hinders understanding on the problem in a whole perspectiveand finding a reasonable solution to our problem. In this study, we present a methodology which can analyze and assess capability utilizing the weapon score of JICM(Joint Integrated Contingency Model). The process identifies capability gap from a mission-oriented perspective in the requirement planning phase and suggests an appropriate solution to our problem. A Quick Look tool which has been developed using Python Script to implement the methodology is also introduced in this study.

Genetic algorithm based multi-UAV mission planning method considering temporal constraints (시간 제한 조건을 고려한 유전 알고리즘 기반 다수 무인기 임무계획기법)

  • Byeong-Min Jeong;Dae-Sung Jang;Nam-Eung Hwang;Joon-Won Kim;Han-Lim Choi
    • Journal of Aerospace System Engineering
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    • v.17 no.2
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    • pp.78-85
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    • 2023
  • For Multi-UAV systems, a task allocation could be a key factor to determine the capability to perform a task. In this paper, we proposed a task allocation method based on genetic algorithm for minimizing makespan and satisfying various constraints. To obtain the optimal solution of the task allocation problem, a huge calculation effort is necessary. Therefore, a genetic algorithm-based method could be an alternative to get the answer. Many types of UAVs, tasks, and constraints in real worlds are introduced and considered when tasks are assigned. The proposed method can build the task sequence of each UAV and calculate waiting time before beginning tasks related to constraints. After initial task allocation with a genetic algorithm, waiting time is added to satisfy constraints. Multiple numerical simulation results validated the performance of this mission planning method with minimized makespan.

Design of the COMS Satellite Ground Control System (통신해양기상위성 관제시스템 설계)

  • Lee, Byeong-Seon;Jeong, Won-Chan;Lee, Sang-Uk;Lee, Jeom-Hun;Kim, Jae-Hun
    • Journal of Satellite, Information and Communications
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    • v.1 no.2
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    • pp.16-24
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    • 2006
  • As a multi-mission GEO satellite, COMS system is being developed jointly by KARI, ETRI, KORDI, KMA, and industries from both abroad and domestic. EADS ASRTIUM is the prime contractor for manufacturing the COMS. ETRI is developing the COMS Ka-band payload and SGCS with the fund from MIC. COMS Satellite Ground Control System (SGCS) will be the only system for monitor and control of the satellite in orbit. In order to fulfill the mission operations of the three payloads and spacecraft bus, COMS SGCS performs telemetry reception and processing, satellite tracking and ranging, command generation and transmission, satellite mission planning, flight dynamics operations, and satellite simulation, By the proper functional allocations, COMS SGCS is divided into five subsystems such as TTC, ROS, MPS, FDS, and CSS. In this paper, functional design of the COMS SGCS is described as five subsystems and the interfaces among the subsystems.

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OPTIMUM AKN BURN PLANNING FOR ORBITAL TRANSFER OF KOREASAT (무궁화 위성의 궤도전이를 위한 최적 원지점 점화 계획)

  • 송우영;최규홍
    • Journal of Astronomy and Space Sciences
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    • v.11 no.2
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    • pp.296-307
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    • 1994
  • Using X-Window system (Motif Graphic User Interface), the AKM (Apogee Kick Motor) firing software for Koreasat which will be launched in 1995 has been developed to transfer the spacecraft from its transfer orbit, provided by the DeltaII launch vehicle, into a nearly geostationary drift orbit. The AKM firing software runs in one of two modes. In mission analysis mode, using a fixed magnitude impulsive velocity change, it provides the necessary data for planning the burn parameters. In insert mode, it uses the orbit propagator function to integrate the spacecraft state through the AKM burn. In this case, an AKM thrust profile and specific impulse are applied to the necessary data for planning the burn parameters to obtain the best possible drift orbit. The apogee burn planning simulation for orbital transfer of Koreasat has been performed using the AKM firing software. And the result of this simulation has been analyzed.

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Route Planning and Elevator Boarding Algorithms for Last Mile Delivery Service in Multi-floor Environments (다층 환경에서의 라스트 마일 배송 서비스를 위한 경로 계획 및 엘리베이터 탑승 알고리즘)

  • Daegyu Lee;Gyuree Kang;Taejin Kim;D. Hyunchul Shim;Hoon Jung;Eunhye Kim
    • The Journal of Korea Robotics Society
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    • v.18 no.1
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    • pp.10-17
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    • 2023
  • Recently, robots have been actively utilized for logistics and delivery services in various places such as restaurants, hotels, and hospitals. In addition, it provides a safer environment, convenience, and cost efficiency to the customers. However, when it comes to autonomous delivery in a multi-floor environment, the task is still challenging. Especially for wheeled mobile robots, it is necessary to deal with elevators to perform the last-mile delivery services. Therefore, we present a multi-floor route planning algorithm that enables a wheeled mobile robot to traverse an elevator for the delivery service. In addition, an elevator boarding mission algorithm was developed to perceive the drivable region within the elevator and generate a feasible path that is collision-free. The algorithm was tested with real-world experiments and was demonstrated to perform autonomous postal delivery service in a multi-floor building. We concluded that our study could contribute to building a stable autonomous driving robot system for a multi-floor environment.

A Development of Simulation System for 3D Path Planning of UUV (무인잠수정의 3차원 경로계획을 위한 시뮬레이션 시스템 개발)

  • Shin, Seoung-Chul;Seon, Hwi-Joon
    • Proceedings of the Korean Institute of Information and Commucation Sciences Conference
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    • 2010.10a
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    • pp.701-704
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    • 2010
  • In studying an autonomous navigation technique of UUV(Unmaned Underwater Vehicle), one of the many fundamental techniques is to plan a 3D path to complete the mission via realtime information received by sonar showing landscapes and obstacles. The simulation system is necessary to verify the algorithm in researching and developing 3D path planning of UUV. It is because 3D path planning of UUV should consider guide control, the dynamics, ocean environment, and search sonar models on the basis of obstacle avoidance technique. The simulation system developed in this paper visualizes the UUV's movement of avoiding obstacles, arriving at the goal position via waypoints by using C++ and OpenGL. Plus, it enables the user to setup the various underwater environment and obstacles by a user interface. It also provides a generalization that can verify path planning algorithm of UUV studied in any developing environment.

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Measure of Effectiveness Analysis for Tracking in SONAR System (소나시스템에서의 추적효과도 분석)

  • Cho, Jung-Hong;Kim, Hyoung Rok;Kim, Seongil;Kim, Jea Soo
    • Journal of the Korea Institute of Military Science and Technology
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    • v.16 no.1
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    • pp.5-26
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    • 2013
  • Since the optimized use of sonar systems for target tracking is a practical problem for naval operations, the measure of mission achievability is needed for preparing efficient sonar-maneuver tactic. In order to quantify the mission achievability or Measure Of Effectiveness(MOE) for given sonar-maneuver tactics, we developed and tested a simulation algorithm. The proposed algorithm for tracking is based on Measure Of Performance(MOP) for localization and tracking system of sonar against target. Probability of Detection(PD) using steering beam patterns referenced to the aspect angle of sonar is presented to consider the tracking-performance of sonar. Also, the integrated software package, named as Optimal Acoustic Search Path Planning(OASPP) is used for generating sonar-maneuver patterns and vulnerability analysis for a given scenario. Through simulation of a simple case for which the intuitive solution is known, the proposed algorithm is verified.