• 제어로봇시스템학회:학술대회논문집
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• 제어로봇시스템학회 2001년도 ICCAS
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• pp.56.1-56
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• 2001

Initial attitude error is one of the large error sources in the navigation errors of SDINS. And it is important to decide the initial attitude of SDINS. The method, like a self-alignment or a transfer alignment method, is required to a precise INS. If we do not have a precise INS, we should get large attitude error. After performing the initial alignment, a vehicle has the initial attitude error. Therefore, it results in navigation error due to the initial attitude error. But, if we use position information during flight, we could estimate and compensate a vehicle attitude error. So, we can maintain a precise attitude in spite of existing the initial attitude error. Using the uplinked position information from a land-based radar system, the new algorithm estimates the attitude of the SDINS during flight ...

• 제어로봇시스템학회:학술대회논문집
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• 제어로봇시스템학회 1997년도 한국자동제어학술회의논문집; 한국전력공사 서울연수원; 17-18 Oct. 1997
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• pp.1864-1866
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• 1997

Uncertainties in the aerodynamic coefficients or time delay effects in implementing an autopilot algorithm can make a Flight Control System(FCS) unstable. When a FCS enters unstable state, the actuator or sensor limiters in FCS make the unstable system not diverge but be in the state of stable limit cycle. If an autopilot recognize the FCS to be in the stable limit cycle phenomenon, it woudl be better to adjust autopilot gains to stabilize the FCS. A novel method to stabilize a FCS using parameter estimation and maintenance of given phase margin is proposed. The method is applied to roll control loop and verified its performance.

• 한국항공운항학회지
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• 제29권4호
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• pp.1-20
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• 2021

Due to the recent rapid increase in passenger and cargo air transport demand, the capacity of Jeju International Airport has been approaching its limit. Even though in COVID-19 crisis which has started from Nov 2019, Jeju International Airport still suffers from strong demand in terms of air passenger and cargo transportation. However, it is an undeniable fact that the delay has also increased in Jeju International Airport. In this study, we analyze the correlation between weather and delayed departure operation based on both datum collected from the historical airline operation information and aviation weather statistics of Jeju International Airport. Adopting machine learning techniques, we then analyze weather condition Jeju International Airport and construct a delay prediction model. The model presented in this study is expected to play a useful role to predict aircraft departure delay and contribute to enhance aircraft operation efficiency and punctuality in the Jeju International Airport.

• KSII Transactions on Internet and Information Systems (TIIS)
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• 제14권2호
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• pp.595-609
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• 2020

In this study, we propose a decentralized mathematical model for predictive control of a system of multi-autonomous unmanned aerial vehicles (UAVs), also known as drones. Being decentralized and autonomous implies that all members make their own decisions and fly depending on the dynamic information received from other unmanned aircraft in the area. We consider a variety of realistic characteristics, including time delay and communication locality. For this flocking flight, we do not possess control for central data processing or control over each UAV, as each UAV runs its collision avoidance algorithm by itself. The main contribution of this work is a mathematical model for stable group flight even in adverse weather conditions (e.g., heavy wind, rain, etc.) by adding Gaussian noise. Two of our proposed variance control algorithms are presented in this work. One is based on a simple biological imitation from statistical physical modeling, which mimics animal group behavior; the other is an algorithm for cooperatively tracking an object, which aligns the velocities of neighboring agents corresponding to each other. We demonstrate the stability of the control algorithm and its applicability in autonomous multi-drone systems using numerical simulations.

• 한국항공운항학회:학술대회논문집
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• 한국항공운항학회 2005년도 추계학술발표대회 논문집
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• pp.11-14
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• 2005

• 한국군사과학기술학회지
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• 제13권4호
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• pp.708-715
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• 2010

In Strapdown Inertial Navigation System, alignment accuracy is the most important factor to determine the performance of navigation. However by an existing self-alignment method, it takes a long time to acquire the alignment accuracy that we want. So, to attain the desired alignment accuracy in as little as $\bigcirc$ minutes, we have developed the precise multi-position alignment method. In this paper, it is proposed a inertial measurement matching transfer alignment method among alignment methods to minimize the alignment error in a short time. It is based on a mixed velocity-DCM matching method be suitable to the operating environment of vertical launching system. The compensation methods to reduce misalign error, especially azimuth angle error incurred by measurement time-delay error and body flexure error are analyzed and evaluated with simulation. This simulation results are finally confirmed by experimentations using FMS(Flight Motion Simulator) in Lab and the integration test to follow the fire control mission.

• 제어로봇시스템학회:학술대회논문집
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• 제어로봇시스템학회 1996년도 한국자동제어학술회의논문집(국내학술편); 포항공과대학교, 포항; 24-26 Oct. 1996
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• pp.763-766
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• 1996

A model helicopter is an unstable, multi-input multi-output nonlinear system exposed to strong disturbances and its system parameters change continually. In this paper, Time Delay Control(TDC) is adopted for these reasons. TDC uses past observation of the system's response and the control input to directly modify the control action rather than adjusting the controller gains leading to a model independent robust controller. TDC can force the plant to follow an appropriate reference model, but the reference model cannot be chosen arbitrarily. In this paper the procedure of choosing a reference model and the performance of the controller are presented.

• 한국전자파학회논문지
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• 제28권3호
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• pp.208-216
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• 2017

본 논문은 주파수 변조 연속파(FMCW) 전파고도계의 성능평가를 위한 전파고도계 시뮬레이터 설계 및 개발 내용에 관한 것이다. 전파고도계 시뮬레이터는 전파고도계의 송신 신호를 인가받아 표적과의 거리에 해당하는 만큼 시간 지연된 가상의 수신 신호를 만들어 주는 역할을 하는데, 본 논문에서는 종래의 전파지연 방식인 RF 지연방식의 기술적 한계를 극복하여 광섬유를 지연소자로 활용함으로써 실제 비행고도에 맞는 다양한 고도의 모의를 가능하게 하였다. 또한, 실제 비행 환경에서 발생할 수 있는 도플러 천이(Doppler shift) 및 재밍(jamming)을 모의할 수 있도록 시뮬레이터를 설계하였다. 개발한 시뮬레이터의 성능은 자체 성능평가 및 전파고도계 연동시험을 통해 성공적으로 검증하였다.

• 한국컴퓨터정보학회논문지
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• 제10권4호
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• pp.285-293
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• 2005

이동 멀티캐스트 환경에서 핸드오프는 이동 단말이 새로운 영역으로 이동할 때 마다 핸드오프와 멀티캐스트 그룹가입을 수행하는 방식으로 일정한 지연시간을 갖게 되며 이동환경에서 핸드오프 지연시간은 패킷 손실을 발생시켜 이동 단말의 수신 품질에 영향을 미치는 주된 요인이 된다. 본 논문에서는 IPv6 환경에서 낮은 핸드오프지연 시간을 갖는 핸드오프 기법을 제안한다. 제안한 핸드오프 기법은 기존의 멀티캐스트의 동작절차를 따르며 인접한 서브넷을 멀티캐스트 트리로 구성하여 단말이 이동할 때 발생하는 멀티캐스트 지연시간을 감소시켜 패킷손실을 제거하였다. 모의실험을 통해 제안한 기법이 낮은 지연시간을 갖는 것을 확인하였으며 원격가입 방식보다 작은 패킷 손실률을 보였다.

• 한국항행학회논문지
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• 제21권1호
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• pp.36-42
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• 2017

공항 내에서의 효율적인 지상 교통 관리를 위하여 선입-선처리 (FCFS; first-come first-served) 알고리즘을 적용한 항공기 지상 이동 스케줄러를 개발하였다. 본 스케줄러는 이전에 개발한 공역 내 교통 흐름 관리 스케줄러를 기반으로 하며, 지상 이동에 있어 추가적으로 요구되는 제약 조건인 링크의 방향성과 교차로 처리 등을 추가하였다. 추가된 각각의 제약 조건을 만족하는지 검증하기 위해 단순한 시나리오를 제작하여 시뮬레이션을 수행하였으며, 시뮬레이션 결과가 주어진 제약 조건을 만족하는 것을 확인하였다. 또한 제주 공항의 실제 항공기 출 도착 데이터인 FOIS (flight operation information system) 데이터를 기반으로 시나리오를 제작하여 시뮬레이션을 진행하였다. 개발한 스케줄러의 실효용성을 판단하기 위해, 실제 평균 지연시간과 스케줄러를 통해 산출한 평균 지연 시간을 비교하였다.