• 제어로봇시스템학회논문지
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• 제16권2호
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• pp.177-187
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• 2010

A MTG (Multimode Tracking and Guidance) system is employed to compensate for the limitations of individual seekers such as RF (Radio frequency) or IIR (Imaging Infra-red) and to improve the overall tracking and guidance performance in jamming, clutter, and adverse weather environments. In the MTG system, tracking filter, data association, and data fusion methods are important elements to maximize the effectiveness of precision homing missile guidance. This paper proposes the formulation of a Kalman filter for the estimation of line-of-sight rate from seeker measurements in missiles guided by proportional navigation. Also, we suggest the HPDA (Highest Probability Data Association) and data fusion methods of the MTG system for target tracking in the adverse environments. Mont-Carlo simulation is employed to evaluate the overall tracking performance and guidance accuracy.

• 전기학회논문지
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• 제68권4호
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• pp.566-572
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• 2019

This paper proposes a new composite guidance law that can intercept moving targets and satisfy look angle rate constraint. In order to obtain the composite guidance law, we first develop a new look angle rate control guidance law which can maintain the maximum look angle rate limitation. And then, we propose the composite guidance scheme on the basis of the look angle rate control guidance and the proportional navigation guidance. To investigate the capturablity and characteristics of the proposed guidance, we also derive closed-form solutions and perform various numerical simulations. The proposed composite guidance only requires the line-of-sight rate, closing velocity, and missile's speed, thereby easily implementing in practical homing missiles.

• 한국항공우주학회지
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• 제43권6호
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• pp.497-506
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• 2015

본 논문은 기동이 없는 이동표적에 대하여 탐색기의 FOV(field-of-view) 및 기동가속도 제한 내에서 충돌각 제어를 위한 복합 유도법칙을 제안한다. 제안하는 유도법칙은 비례 항법(proportional navigation)의 특성을 이용하는 것으로 총 두 단계의 유도 명령을 생성하게 된다. 첫 번째 유도명령은 초기 유도단계에서 표적에 대한 지향각(look angle)을 일정하게 유지하게 하고, 특정한 시선각 조건을 만족하면 두 번째 비례 항법 유도로 전환하여 원하는 충돌각으로 표적을 타격하게 된다. 충돌각 설정을 용이하게 하기 위하여 제한된 유도탄의 성능 조건을 가지고 달성 가능한 최대 충돌각 계산방법을 제시한다. 수치 시뮬레이션을 통해 설계된 유도법칙의 성능 및 실제 유도탄 환경에 대한 적용가능성을 분석한다.

• 한국항공우주학회지
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• 제46권9호
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• pp.742-751
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• 2018

본 논문은 지대지 교전상황에서 유도탄 탐색기의 Field-of-View(FOV)와 가속도 제한을 고려하여 충돌각을 제어하는 시변 편향 비례항법 유도법칙(Time Varying Biased Proportional Navigation Guidance Law)을 제안하고 있다. 제안한 유도법칙은 FOV 제한을 고려하여 3단계로 구성이 되는데 각 단계에서 편향이 가속도에 직접적인 영향을 미치기 때문에 편향을 생성하는데 있어서 단계가 넘어갈 때 전 단계의 마지막 편향이 다음 단계의 시작 편향이 되도록 하였다. 또한, 교전 상황과 물리적 구속조건을 고려하여 충돌각 도달 여부를 판단하는 로직 또한 설명하고 있다.

• 한국시뮬레이션학회논문지
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• 제19권4호
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• pp.209-218
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• 2010

합성 환경/실험 체계 전술객체 표현 기술 연구는 전술객체들의 위치를 실시간으로 탐지·추적하고 이를 가상현실 내에서 모의하기 위한 기반 기술을 확보하는 것을 목적으로 한다. 이를 위한 기술로써 전술객체 위치 추적 및 모의 기술, 모델 간 공유기술에 대한 연구가 필요하다. 본 논문에서는 우선 센서 데이터 융합과 좌표계 통일을 위한 알고리즘을 연구하였고, 추적자의 유도 방식인 PNG(Proportional Navigation Guidance)를 적용한 추적 기술, 공학급 및 상급 모델의 회피 알고리즘을 적용한 회피 기술을 연구하였다. 또한, 잠수함과 어뢰의 추적 회피 시뮬레이션을 통해 전술객체의 위치 모의를 연구하였다.

• 제어로봇시스템학회:학술대회논문집
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• 제어로봇시스템학회 1992년도 한국자동제어학술회의논문집(국내학술편); KOEX, Seoul; 19-21 Oct. 1992
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• pp.584-589
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• 1992

The 3-dimensional PPNG(Pure proportional navigation guidance) law was proposed about forty years ago, but the satisfactory analysis of its performance has not been presented since then. In this note, we prove under some reasonable assumptions that the missile guided according to this 3-dimensional PPNG law can always intercept a randomly maneuvering target if (1) the target acceleration varies with a certain bound, (2) the navigation constant is selected large and (3) the initial heading error is small. We introduce a Lyapunov-like method that proves to be a very powerful tool in obtaining our results.

• 한국군사과학기술학회지
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• 제9권4호
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• pp.71-80
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• 2006

Strapdown Inertial navigation systems consist of an inertial sensor assembly(ISA), electronic modules to process sensor data, and a navigation computer to calculate attitude, velocity and position. In the ISA, most gryoscopes such as RLGs and FOGs, have digital output, but typical accelerometers use current as an analog output. For a high precision inertial navigation system, sufficient stability and resolution of the accelerometer board converting the analog accelerometer output into digital data needs to be guaranteed. To achieve this precision, the asymmetric error and A/D reset scale error of the accelerometer board must be properly compensated. If the relation between the acceleration error and the errors of boards are exactly known, the compensation and estimation techniques for the errors may be well developed. However, the A/D Reset scale error consists of a pulse-train type term with a period inversely proportional to an input acceleration additional to a proportional term, which makes it difficult to estimate. In this paper, the effects on the acceleration output for auto-pilot situations and the effects of A/D reset scale errors during horizontal alignment are qualitatively analyzed. The result can be applied to the development of the real-time compensation technique for A/D reset scale error and the derivation of the design parameters for accelerometer board.

• 한국항해항만학회지
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• 제44권2호
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• pp.136-143
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• 2020

Maritime autonomous surface ships (MASS) has been developed over the years. But, there are many unresolved problems. To overcome these problems, this study proposes connected ship navigation system. The system comprises a slave ship and a master ship that leads the slave ship. To implement this system, communication network, route planning algorithms, and controllers are designed. The communication network is built using the transmission control protocol/Internet protocol (TCP/IP) socket communication method to exchange data between ships. The route planning algorithms calculate the course and distance of the slave ship using the middle latitude sailing method. Nomoto model is used as the mathematical model of the slave ship maneuvering motion. Then, the autoregressive with exogenous variables (ARX) model is used to estimate the parameters of Nomoto model. Based on the above model, the automatic steering controller is designed using a proportional-derivative (PD) control. Also, the speed controller is designed for the slave ship to maintain constant distance from the master ship. Sea experiments are conducted to verify the proposed system with two remodeled boats.

• 한국항해항만학회:학술대회논문집
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• 한국항해항만학회 2006년도 International Symposium on GPS/GNSS Vol.1
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• pp.333-335
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• 2006

Position of surface objects can be fixed in many ways. The most popular radionavigational systems, including satellite systems, make possible obtaining nearly continuous and very precise ship's position. However, under the water application of radionavigational systems is impossible. Underwater navigation requires other tools and solutions then these encountered in surface and air navigation. In underwater environment vehicles and submarines, operate that have to possess alternative navigational systems. Underwater vehicles, in order to perform their tasks require accurate information about their own, current position. At present, they are equipped with inertial navigational systems (INS). Accuracy of INS is very high but in relatively short periods. Position error is directly proportional to time of working of the system. The basic feature of INS is its autonomy and passivity. This characteristic mainly decides that INS is broadly used on submarines and other underwater vehicles. However, due to previously mentioned shortcoming i.e. gradually increasing position error, periodical calibration of the system is necessary. The simplest calibration method is surface or nearly surface application of GPS system. Another solution, which does not require interruption of performed task and emergence on the surface, is application of comparative navigation technique. Information about surrounding environment of the ship, obtained e.g. by means sonic depth finder or board sonar, and comparing it with accessible pattern can be used in order to fix ship's position. The article presents a structure and a description of working of underwater vehicle navigation system simulator. The simulator works on the basis of comparative navigation methods which exploit in turn digital images of echograms and sonograms. The additional option of the simulator is ability to robust estimation of measurements. One can do it in order to increase accuracy of position fixed with comparative navigation methods application. The simulator can be a basis to build future underwater navigation system.

• 제어로봇시스템학회:학술대회논문집
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• 제어로봇시스템학회 2001년도 ICCAS
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• pp.64.3-64
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• 2001

In this paper, an estimation scheme with the IMM algorithm to estimate radome slope and target states is used to reduce the radome induced miss distance effectively in spatial active homing engagements of an anti-air missile. The filter algorithm in conjunction with proportional navigation guidance is tested by a series of simulation runs.