• 제어로봇시스템학회논문지
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• 제8권1호
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• pp.60-66
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• 2002

In this paper, a new target pointing guidance algorithm is proposed by combining the optimal target pointing solution and a simple time-to-Go estimator. Also investigated are some properties of the guidance algorithm which include a relation to conventional PNG, convergence region and convergence trajectories of error states according to the time-to-go estimator gain. Some guidelines for designing the pointing guidance law are commented based on the convergence properties. A design example in the case of large initial heading errors is presented and its performance is investigated by simulation.

• 제어로봇시스템학회논문지
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• 제14권8호
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• pp.740-744
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• 2008

In this paper, we propose a new time-to-go estimation filter for PN guided missiles. The proposed estimator is derived based on the approximation of the length of the PNG homing trajectory that we newly introduced using the special coordinate system. The coordinate system is convenient for taking the target movement into account. In addition, compared with the previous time-to-go estimation techniques, the parameters required for evaluating the length can be obtained only with the seeker measurements. Moreover, the seeker measurement error statistics can effectively be considered since our filter is derived based on the Kalman filter theory. Simulation result for a typical anti-ship see-skimming missile homing trajectory shows the excellent performance of the proposed filter.

• 대한전자공학회논문지SP
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• 제38권5호
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• pp.509-517
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• 2001

전역탐색알고리즘(full-search algorithm, FSA)은 탐색영역의 범위가 커짐에 따라 방대한 양의 계산을 필요로 하기 때문에 이에 따른 알고리듬의 처리시간이 커지고, 하드웨어로 구현했을 때 회로가 복잡해진다는 문제점을 안고 있다. 본 논문에서는 이러한 문제점을 개선하기 위한 방안으로 비트플레인 정합에 의한 움직임 추정기의 VLSI 구조를 제안한다. 제안된 움직임 추정기에서는 비트 플레인 정합기준을 이용하여 기존의 전역 탐색 알고리즘을 하나의 이진영상으로 적용함으로써 움직임 추정에 소요되는 연산의 양을 크게 줄이면 서도 전역탐색 알고리듬과 유사한 움직임 추정 성능을 갖도록 하였으며, 제안된 VLSI 구조에서는 두 개의 프로세싱 코어를 채택하여 데이터 흐름을 시스톨릭 (systolic) 어레이의 형태로 제어하여, 시스템 내부의 SRAM을 제거하여 동작 속도 상의 이득뿐만 아니라, 메모리 공정을 필요로 하지 않는 저가의 공정을 사용 가능하게 함으로써 제작상의 비용을 절감할 수 있는 해결책을 제시하였다. 구현된 하드웨어는 VHDL을 이용하여 설계하고, 기능 검증을 수행한 후 0.6-μm three-metal CMOS 공정을 이용하여 8.15 X 10.84㎟의 크기로 집적하였다.

• 한국군사과학기술학회지
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• 제5권3호
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• pp.113-119
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• 2002

A target adaptive guidance(TAG) algorithm is proposed employing the near-zone signal that can be measured from an infrared seeker. The guidance order is composed of a conventional PNG command and an additional command to be calculable from an additional LOS rate between a hot point of target and a required intercept point. The characteristic of the near-zone signal is similar to that of LOS rate that is inversely proportional to the square of time-to-go. Hence the proposed scheme can be applied to real systems with no estimator for time-to-go. From analysis results on the miss distance with perfect missile and perfect seeker, it follows that the proposed TAG algorithm guarantees missile to be ideally guided to the required intercept point. And it is less affected by the TAG start time and a proportional navigation ratio than other TAG schemes using a LOS rate such as a step bias or a ramp bias.