• Title/Summary/Keyword: Design guidance

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A study for levitation and guidance control system design

  • Kim, Kook-Hun;Kim, Jong-Moon;Cho, Chang-Hee;Kim, Choon-Kyung
    • 제어로봇시스템학회:학술대회논문집
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    • 1992.10b
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    • pp.532-538
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    • 1992
  • Control system design for attraction type Maglev system is dealt in this paper. Characteristics of levitation and guidance control is explained and a kind of active guidance controller performance is compared with passive guidance control. Also, a method of using absolute and relative information simultaneously is adopted for levitation control. All the methods studied performed very well in the experiments as well as simulation.

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POLYNOMIAL FUNCTION BASED GUIDANCE FOR IMPACT ANGLE AND TIME CONTROL

  • KIM, TAE-HUN
    • Journal of the Korean Society for Industrial and Applied Mathematics
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    • v.19 no.3
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    • pp.305-325
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    • 2015
  • In this paper, missile homing guidance laws to control the impact angle and time are proposed based on the polynomial function. To derive the guidance commands, we first assume that the acceleration command profile can be represented as a polynomial function with unknown coefficients. After that, the unknown coefficients are determined to achieve the given terminal constrains. Using the determined coefficients, we can finally obtain the state feedback guidance command. The suggested approach to design the guidance laws is simple and provides the more generalized optimal solutions of the impact angle and time control guidance.

Rotorcraft Waypoint Guidance Design Using SDRE Controller

  • Yang, Chang-Deok;Kim, Chang-Joo;Yang, Soo-Seok
    • International Journal of Aeronautical and Space Sciences
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    • v.10 no.2
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    • pp.12-22
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    • 2009
  • This paper deals with the State-Dependent Riccati Equation (SDRE) Technique for the design of rotorcraft waypoint guidance. To generate the flight trajectory through multiple waypoints, we use the trigonometric spline. The controller design and its validation is based upon a level 2 simulation rotorcraft model and the designed SDRE controller is applied to the trajectory tracking problems. To verify the designed guidance law, the simulation environment of high fidelity rotorcraft model is developed using three independent PCs. This paper focuses on the validation of rotorcraft waypoint guidance law which is designed by using SDRE Controller.

A Study on the Efficiency of Evacuation Guidance and Non-evacuation Guidance in Case of Fire

  • Ko, Eun-young;Hong, Sung-Ho;Cha, Jae-sang
    • International Journal of Advanced Culture Technology
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    • v.8 no.1
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    • pp.243-247
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    • 2020
  • In the era of the fourth industrial revolution, safety of disasters is being emphasized above all else, and electric fires are most frequent during disasters, and human and property damage is very serious. In this paper, we propose a study that can determine the efficiency of evacuation and non-evacuation guidance due to the large difference in casualties depending on the traffic line in the case of fire. Evacuation guidance was assumed to be a situation in which adequate evacuation routes were guided by a recorded voice or a trained staff, and non-evacuation guidance was assumed to be a situation without anything. Evacuation simulations were carried out using a evacuation simulation tool called PATHFINDER and SIMULEX for the analysis of the efficiency of evacuation and non-evacuation guidance. As a result, the evacuation time was similar, but in the case of non-evacuation guidance, it was not guided to the safe zone, which could cause serious damage.

Design of Public Transportation Route Guidance System for Wheelchair Users Utilizing Public Data of Seoul City

  • Geumbi, Lee;Humberto, Villalta;Seunghyun, Kim;Kisu, Kim;Jaehyeong, Go;Yongjoo, Jun;Kwang Sik, Kim
    • International Journal of Internet, Broadcasting and Communication
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    • v.15 no.1
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    • pp.97-112
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    • 2023
  • The purpose of this study is to design and test a new way of public transportation route guidance system for persons with disabilities, including wheelchair users. The guidance system is smartphone app-based, using, routes that involve disabled-friendly facilities in the vicinity can be searched. A database that contains publicly available data on low-floor bus services, location and extent of disabled-friendly facilities, and suitable subways and stations, was developed for this purpose. The app uses the database to access and query the required information. A pilot study was conducted to test the effectiveness of the guidance system. It was found that the system was able to convey information about the disabled-friendly routes and related guidance information even inside subway stations, effectively. The performance of the system was compared with route guidance services that do not explicitly use data on disabled-friendly services. A notable difference was observed in the travel time estimated by this program and other guidance services. The difference was around 4 to 15 minutes. This is significant savings for persons with disabilities if they use the app and service. The study thus shows that exclusive use of disabled-friendly data in route guidance will bring more benefits for persons with disabilities.

Considerations in Practical Advanced Guidance Law Development (실용적 첨단유도법칙 개발을 위한 고려사항)

  • 조항주
    • Journal of the Korea Institute of Military Science and Technology
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    • v.5 no.1
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    • pp.96-106
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    • 2002
  • Many modern guided weapon systems employ sophisticated target sensors as well as powerful computing systems. Due to such advanced features, they are required to achieve better guidance accuracy, and at the same time other guidance objectives for better weapon effectiveness and survivability. In this paper, we overview some of the technical considerations in such advanced guidance algorithm development, and briefly look at some related research works. More specifically, we discuss impact angle control, time-varying nature of the guidance system, time-to-go estimation, guidance loop stability, effect of autopilot lag and physical limitations in control variables, parasitic paths in guidance loops, etc. We also briefly look at some advanced concepts such as integrated guidance and control loop design, target adaptive guidance, guidance law development based on dual control concept, and terminal evasive maneuver.

A Novel Nonlinear Robust Guidance Law Design Based On SDRE Technique

  • Moosapour, Seyyed Sajjad;Alizadeh, Ghasem;Khanmohammadi, Sohrab;Moosapour, Seyyed Hamzeh
    • International Journal of Aeronautical and Space Sciences
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    • v.13 no.3
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    • pp.369-376
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    • 2012
  • A nonlinear robust guidance law is designed for missiles against a maneuvering target by incorporating sliding-mode and optimal control theories based on the state dependent Riccati equation (SDRE) to achieve robustness against target accelerations. The guidance law is derived based on three-dimensional nonlinear engagement kinematics and its robustness against disturbances is proved by the second method of Lyapunov. A new switching surface is considered in the sliding-mode control design. The proposed guidance law requires the maximum value of the target maneuver, and therefore opposed to the conventional augmented proportional navigation guidance (APNG) law, complete information about the target maneuver is not necessary, and hence it is simple to implement in practical applications. Considering different types of target maneuvers, several scenario simulations are performed. Simulation results confirm that the proposed guidance law has much better robustness, faster convergence, and smaller final time and control effort in comparison to the sliding-mode guidance (SMG) and APNG laws.

Detail-design Guidance for the Openings on the Web Structure Supporting the Deck (갑판지지 웨브 구조에서의 개구부 상세설계기준 정립)

  • Kim, Sung-Chan;Lee, Kyung-Seok;Song, Jae-Young;Kim, Kyung-Su
    • Journal of the Society of Naval Architects of Korea
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    • v.44 no.6
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    • pp.612-618
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    • 2007
  • There are a lot of openings, holes and slots in ship structural members. It is not easy to solve the troubles around the openings adequately at the detail design stage, because there are a lot of concerning locations. There are not also clear design rules of classification societies and it is not possible to apply direct calculation for all the concerning members. Therefore, it is necessary to set up simplified approach such as a standard or guidance in order to decide the opening design quickly. For this study, guidance and regulations of each classification and several companies were surveyed. Grillage analysis and the refined mesh method were used to evaluate the strength around hole considering boundary condition and more detailed member arrangement. As a result, the standard for opening design was established and verified.

Building guidance-sign system to improve efficiency of waste separate collection at movie theatres - Focusing on Megabox Movie Theater in Seoul - (국내 영화관의 효율적인 쓰레기 분리수거 촉진을 위한 사인 디자인 체계 연구 - 메가박스 사례를 중심으로 -)

  • Paik, Jinkyung;Hwang, Sangmi;Chun, Eunyoung
    • Design Convergence Study
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    • v.14 no.4
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    • pp.53-64
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    • 2015
  • The purpose of this research is to examine and find solutions with garbage problems in movie theaters for the betterment of pleasant environment to customers. The object of investigation includes three most popular movie theaters in Seoul. Analyzing current status of separating garbage and guidance notice was carried out. Also investigation of awareness on separating garbage and guidance notice has been done. The findings on inquiry are as follows. Customers tend not to separate garbage and guidance notice was not as effective. Also, separate garbage collection was very ineffective especially the food garbage. We carried out investigation on placement of guidance notice regarding recycling bin. We tried to find solutions for this problem and proposed better design. This design is emphasized on the use of particular space only. In addition, this design is focused mainly on one the three movie theaters for integration of identity. Through this design, it ought to provide clean environment and reduces inefficiencies regarding financial and time.

Automatic Landing Guidance Law Design for Unmanned Aerial Vehicles based on Pursuit Guidance Law (추적유도기법 기반 무인항공기 자동착륙 유도법칙 설계)

  • Yoon, Seung-Ho;Bae, Se-Lin;Han, Young-Soo;Kim, Hyoun-Jin;Kim, You-Dan
    • Journal of Institute of Control, Robotics and Systems
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    • v.14 no.12
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    • pp.1253-1259
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    • 2008
  • This paper presents a landing controller and guidance law for net-recovery of fixed-wing unmanned aerial vehicles. A linear quadratic controller was designed using the system identification result of the unmanned aerial vehicle. A pursuit guidance law is applied to guide the vehicle to a recovery net with imaginary landing points on the desired approach path. The landing performance of a pure pursuit guidance, a constant pseudo pursuit guidance, and a variable pseudo pursuit guidance is compared. Numerical simulation using an unmanned aerial vehicle model was performed to verify the performance of the proposed landing guidance law.