• International journal of advanced smart convergence
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• 제12권1호
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• pp.31-40
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• 2023

This asymed drone controller is indispensable for two components: Guidance and Controller. In which the Ministry of Guidance will receive waypoints from which to form an orbit then combine the data with the current location of the vessel, thereby calculating and also supplying the controller to drive the vehicle to follow the outlined trajectory. This article will use the Line Of Sight (LOS) algorithm to design the Guidance and Controller sets. The result as well as the effectiveness of the controller will be shown through matlab/SIMULINK simulation.

• 대한전기학회:학술대회논문집
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• 대한전기학회 2002년도 추계학술대회 논문집 전력기술부문
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• pp.47-49
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• 2002

Recently, the power system has a trend of a sustaining growth in electric power demand with large-sized formation. In this situation, current states can be definitely comprehended to operate security and economic power system. Also, corrective actions must be performed for the violation of bus voltage and line overload. In the security and economy with on-line, It is desirable that the situations of violation are promptly removed to operate power system effectively. This paper deals with the development of application, Kangyang Steel Works' Power System Guidance System, for voltage and overload correction on base case using Generator-Voltage Sensitivity List(GVSL) and Generator Shifter Factor List(GSFL). Also, to show the superiority and economical efficiency of the proposed application, we simulate the Kangyang Steel Works' Power System.

• 제어로봇시스템학회논문지
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• 제16권5호
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• pp.498-509
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• 2010

In this paper, a waypoint guidance law Line Tracking algorithm is designed for testing an Unmanned Airship. In order to verify, we develop an autonomous flight control and test system of unmanned airship. The flight test system is composed FCC (Flight Control Computer), GCS (Ground Control System), Autopilot & Guidance program, GUI (Graphic User Interface) based analysis program, and Test Log Sheet for the management of flight test data. It contains flight test results of single-path & multi-path following, one point continuation turn, LOS guidance, and safe mode for emergency.

• 대한전기학회:학술대회논문집
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• 대한전기학회 2005년도 학술대회 논문집 정보 및 제어부문
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• pp.632-634
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• 2005

In this paper, The Frenet-Serret formula of classical geometric curve theory with the concept of a missile pointing velocity vector are used to analyze and design a missile guidance law. The capture capability of this guidance law is qualitatively studied by comparing the rotations of the velocity vectors of missile and target relative to the line of sight vector. when fuzzy Table look-up theory applied in target-missile distance & angle displacement, this research. It's performance is better then classical research.

• 한국항공우주학회지
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• 제48권11호
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• pp.873-880
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• 2020

본 논문은 스트랩다운 탐색기 측정치와 INS 정보를 이용하여 시선각속도를 추정하는 유도필터 설계에 대해서 다룬다. 제안하는 유도필터는 탐색기 측정치와 유도탄 자세로부터 획득 가능한 시선각과 표적의 위치와 유도탄과의 상대 위치를 측정치로 하고 있으며, 주기 및 동기가 맞지 않는 두 센서의 출력을 사용하기 위해 비동기 필터를 기반으로 하고 있다. 제안한 방법을 통해 시간지연이 큰 탐색기 측정치를 사용함으로써 생길 수 있는 기생루프에 대한 영향을 줄이고 추정성능을 향상시킬 수 있다.

• 제어로봇시스템학회:학술대회논문집
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• 제어로봇시스템학회 2001년도 ICCAS
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• pp.141.2-141
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• 2001

An approximate target adaptive guidance algorithm(TAG) is proposed on the basis of the assumption that angular acceleration of missile to target line-of-sight and start time for TAG can be obtained by IR seeker. The algorithm does not use any target state estimator. Instead, it avoids the problem of determining target attitude by using the observation that the missile using LOS rate guidance is nearly on the collision course in the later point of engagement. Computer simulation results show that the proposed algorithm can effectively perform target adaptive guidance.

• 한국정보과학회논문지:시스템및이론
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• 제37권2호
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• pp.110-125
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• 2010

본 논문은 이차원 영상으로부터 시각적으로 효과적인 정보를 제공할 수 있는 라인 드로잉 영상을 생성하는 방법을 제시한다. 본 방법은 기존의 단순한 에지 추출 방법과 달리 사람의 라인 드로잉 과정을 적용하여 직관적이면서 효과적인 결과를 생성하며, 크게 라인 추출, 라인 렌더링, 사용자 지시의 세단계로 구성된다. 라인 추출 단계에서는 우도 함수를 이용하여 물체의 중요한 경계 부분을 효과적으로 예측함으로써 라인을 추출한다. 추출된 라인을 실제 렌더링하는 라인 렌더링 단계에서는, 중요한 라인과 세부 라인의 구분 및 초점의 정확도를 표현하기 위하여 라인의 특징 크기와 번짐 정도를 고려하고, 이를 다양한 스타일로 표현하기 위해 텍스쳐 형태의 라인 영상을 적용한다. 마지막으로 사용자 지시 단계에서는 자동으로 생성된 라인의 모양이나 위치를 사용자 상호작용으로 수정할 수 있다. 이 때 사용자 입력에 대한 즉각적인 반응을 위해 라인 추출의 대부분의 과정이 GPU 상에서 구현된다. 제시된 방법의 결과로 사용자는 이차원 영상으로부터 중요한 부분과 초점이 맞는 부분의 표현 및 스타일을 원하는 대로 조절한 라인 드로잉을 얻을 수 있고, 또한 이를 자유롭게 수정할 수 있다.

• International Journal of Aeronautical and Space Sciences
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• 제15권3호
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• pp.281-292
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• 2014

We propose a novel cooperative guidance law design method based on the finite time disturbance observer (FTDO) for multiple near space interceptors (NSIs) with impact time control. Initially, we construct a cooperative guidance model with head pursuit, and employ the FTDO to estimate the system disturbance caused by target maneuvering. We subsequently separate the cooperative guidance process into two stages, and develop the normal acceleration command based on the super-twisting algorithm (STA) and disturbance estimated value, to ensure the convergence of the relative distance. Then, we also design the acceleration command along the line-of-sight (LOS), based on the nonsingular fast terminal sliding mode (NFTSM) control, to ensure that all the NSIs simultaneously hit the target. Furthermore, we prove the stability of the closed-loop guidance system, based on the Lyapunov theory. Finally, our simulation results of a three-to-one interception scenario show that the proposed cooperative guidance scheme makes all the NSIs hit the target at the same time.

• 제어로봇시스템학회:학술대회논문집
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• 제어로봇시스템학회 2003년도 ICCAS
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• pp.1822-1825
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• 2003

A practical range estimator based on the robust Kalman filter is proposed to solve the range estimation problem for surface to air missile(SAM) homing guidance. Apart from the previous works based on the extended Kalman filter(EKF) with bearing only measurement, the proposed scheme makes use of line-of-sight(LOS) rate to ensure the fast convergency at long-range. In this reason, the robust Kalman filter is considered to deal with LOS rate measurement error. The recursive linear structure of proposed filter is easy to implement and make it possible to reduce computational burdens. Moreover, it shows good estimation performance without specific guidance law such as oscillation proportional navigation guidance(OPNG).

• 제어로봇시스템학회:학술대회논문집
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• 제어로봇시스템학회 2001년도 ICCAS
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• pp.156.3-156
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• 2001

This paper handles synthesis and investigation of a neural network guidance law based on pursuit-evasion games. This work considers two-dimensional pursuit-evasion games solved by using the gradient method. The procedure of developing a guidance law from the game-optimal solutions is deeply examined, and important features of the neural network guidance are investigated. The proposed neural network guidance law takes the range, range rate, line-of-sight rate, and heading error as its input variables. By reconstructing the trajectory, the accuracy of the neural network approximation is verified. Afterwards, robustness of the neural network guidance to the autopilot lag, which results from its feedback structure, is investigated ...