• International Journal of Aeronautical and Space Sciences
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• 제7권2호
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• pp.137-144
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• 2006

The objective of this paper is to present trajectory guidance and control system with a dynamic inversion for a small unmanned aerial vehicle (UAV). The UAV model is expressed by fixed-mass rigid-body six-degree-of-freedom equations of motion, which include the detailed aerodynamic coefficients, the engine model and the actuator models that have lags and limits. A trajectory is generated from the given waypoints using cubic spline functions of a flight distance. The commanded values of an angle of attack, a sideslip angle, a bank angle and a thrust, are calculated from guidance forces to trace the flight trajectory. To adapt various waypoint locations, a proportional navigation is combined with the guidance system. By the decision logic, appropriate guidance law is selected. The flight control system to achieve the commands is designed using a dynamic inversion approach. For a dynamic inversion controller we use the two-timescale assumption that separates the fast dynamics, involving the angular rates of the aircraft, from the slow dynamics, which include angle of attack, sideslip angle, and bank angle. Some numerical simulations are conducted to see the performance of the proposed guidance and control system.

• 한국통신학회논문지
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• 제26권12A호
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• pp.1990-1999
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• 2001

본 논문에서는 단소자 적외선 레티클 탐색기의 단점을 해결하기 위해 적외선의 두 대역을 이용하는 2-color 회전 동심원 레티클 탐색기(concentric annular ring reticle seeker)의 시뮬레이션 툴이 제안된다. 표적 및 섬광탄(flare)의 모델링과 비례항법 유도(proportional navigation guidance) 루프를 포함한 동적인 시뮬레이션 툴 상에서 동심원 레티클 탐색기의 추적 성능과 섬광탄에 의한 영항 등을 분석한다. 또한 다양한 상량에서 운용되는 섬광탄의 영향을 효과적으로 배제하기 위해 LMS 방법을 이용한 새로운 반대응능력(counter-countermeasure)이 제안된다. SWIR 및 MWIR 대역에서 표적과 섬광탄의 상대적 분포특성을 이용함으로써 섬광탄에 효과적으로 대처할 수 있으며, 교전 시나리오에서 기존 반대응 기법과의 비교를 통해 제안된 알고리즘의 향상된 추적 성능을 확인하였다.

• 한국항공우주학회지
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• 제43권8호
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• pp.669-676
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• 2015

본 논문에서는 기동하는 표적에 대한 입사각 제어 유도법칙을 제안하였다. 제안된 유도법칙은 정지표적에 대한 최적입사각제어 유도법칙을 변형한 것으로서 기존의 PN(Proportional Navigation) 유도법칙에 입사각제어 항이 추가된 바이어스 PN 유도법칙의 형태를 갖는다. 시선각, 비행경로각, 그리고 표적에 대한 상대 비행경로각 관점에서의 세 가지 다른 종류의 입사각을 정의하였다. 다양한 공대공 교전 시나리오에 대한 수치 시뮬레이션을 통해 제안한 유도법칙의 성능을 검증하였다.

• 한국항행학회논문지
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• 제14권6호
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• pp.1002-1009
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• 2010

본 논문에서는 축삭의 전도 현상을 분석하기 위해서 축삭을 전기전도 모델로 만든 후 여기에 키르히호프의 전류법칙과 전압법칙을 적용한 등가회로를 구성하였다. 축삭의 미세거리 변화에 의한 전위의 거동을 분석하기 위하여 축삭의 각종 파라미터를 구하였다. 검토결과에 의하면 무수신경인 경우 직경을 미지수로 하여 인체의 파라미터를 이용하면 그 속도는 직경의 제곱근에 비례한다. 한편 유수신경인 경우는 그 속도가 직경에 직접적으로 비례한다. 미엘린이 없는 막과는 달리 미엘린껍질의 전도는 전압과 무관하므로 이러한 막 양단의 Hodgkin-Huxley 형 전도모델이 매우 정교하지는 않다.

• 한국지능시스템학회논문지
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• 제19권5호
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• pp.699-705
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• 2009

본 논문은 지게차 AGV(autonomous ground vehicle)의 자율주행을 위한 제어 방법에 관한 연구이다. 기존에 개발된 지게차 AGV의 위치측정 방법으로는 자기-자이로 유도(magnet-gyro guidance) 방식과 유선 유도(wire guidance) 방법이 있지만, 유지보수에 대한 지속적인 노력과 비용문제가 있으며, 작업 환경의 변화에 따라 작업 환경을 재구성해야하는 단점이 있다. 따라서 본 논문에서는 외란에 강인하고 작업 환경 및 작업 내용의 변경에 유연한 시스템을 구축하기 위해 레이저 내비게이션 센서와 엔코더, 자이로 센서의 센서융합을 통한 위치측정 시스템을 개발하였다. 또한 팔레트를 하역 운송해야하는 지게차 AGV의 주행제어를 위해 팔레트와 지게차 AGV 사이의 거리 차와 각도 차를 바탕으로 퍼지 제어 및 비례 제어를 이용한 주행제어기를 설계하였다. 본 연구에서 제안한 지게차 AGV를 위한 제어 시스템의 성능 분석을 위해 물류 운송작업이 가능한 작업공간에서 동일한 하역 작업을 10회 반복 하였다. 그 결과, 시뮬레이션에 의해 생성된 경로와 실제 주행경로의 최대 평균 오차가 87.77mm를 가짐을 확인하였다.

• 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.

• 한국항해항만학회:학술대회논문집
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• 한국항해항만학회 2006년도 International Symposium on GPS/GNSS Vol.2
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• pp.15-22
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• 2006

This paper presents a novel signal tracking algorithm for GNSS receivers using a MLE technique. In order to perform a robust signal tracking in severe signal environments, e.g., high dynamics for navigation vehicles or weak signals for indoor positioning, the MLE based signal tracking approach is adopted in the paper. With assuming white Gaussian additive noise, the cost function of MLE is expanded to the cost function of NLSE. Efficient and practical approach for Doppler frequency tracking by the MLE is derived based on the assumption of code-free signals, i.e., the cost function of the MLE for carrier Doppler tracking is used to derive a discriminator function to create error signals from incoming and reference signals. The use of the MLE method for carrier tracking makes it possible to generalize the MLE equation for arbitrary codes and modulation schemes. This is ideally suited for various GNSS signals with same structure of tracking module. This paper proposes two different types of MLE based tracking method, i.e., an iterative batch processing method and a non-iterative feed-forward processing method. The first method is derived without any limitation on time consumption, while the second method is proposed for a time limited case by using a 1st derivative of cost function, which is proportional to error signal from discriminators of conventional tracking methods. The second method can be implemented by a block diagram approach for tracking carrier phase, Doppler frequency and code phase with assuming no correlation of signal parameters. Finally, a state space form of FLL/PLL/DLL is adopted to the designed MLE based tracking algorithm for reducing noise on the estimated signal parameters.

• 한국지능시스템학회:학술대회논문집
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• 한국퍼지및지능시스템학회 2003년도 ISIS 2003
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• pp.346-349
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• 2003

For a traveling crane, various control methods such as neural network predictive control and TDOFPID(Two Degree of Freedom Proportional Integral Derivative) are studied. So in this paper, we proposed improved navigation method to reduce transfer time and sway with anti-collision path for avoiding collision in its movement to the finial coordinate. And we constructed the NNPPID(Neural Network Predictive PID) controller to control the precise move and speedy navigation. The proposed predictive control system is composed of the neural network predictor, TDOFPID controller, and neural network self-tuner. We analyzed ASC(Automated Stacking Crane) system and showed some computer simulations to prove excellence of the proposed controller than other conventional controllers.

• International Journal of Aeronautical and Space Sciences
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• 제11권3호
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• pp.184-192
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• 2010

In this paper, an initial fine alignment algorithm, which is developed for the strap-down inertial navigation systems of satellite launch vehicles, is considered. For fast and accurate alignment, a simple closed-loop estimation algorithm using a proportional-integral controller is introduced. Through computer simulation for the sway condition in the launch pad, it is shown that a simple filter structure can guarantee fast computational speed that is adequate for real-time implementation as well as the required alignment accuracy and robustness. In addition, its implementation results are presented for the Naro-1 flight test.

• 한국항해학회지
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• 제25권4호
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• pp.407-415
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• 2001

In the present study, irregular disturbances to ship dynamics is proposed, where irregular disturbances implying irregular wave and the fluctuating component of wind for the evaluation of automatic steering system of ship in following seas. Prediction method based on the principle of linear superposition. Irregular wave disturbances in following seas is calculated by frequency variation method. The mathematical model of each element of an automatic steering system is derived, which takes account of a few non-linear mechanisms. PD(Proportional-Derivative) controller and low-pass filter with a weather adjustment are adopted to modelling the characteristics of an autopilot. Performance index is introduced from the viewpoint of energy saving, which derived from the concept of energy loss on ship propulsion. Finally, the present methods are applied to two typical types of ship ; an ore carrier and a fishing boat. The various effects of control constants of autopilot on propulsive energy loss are investigated