• 한국시뮬레이션학회논문지
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• 제33권2호
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• pp.37-44
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• 2024

한국형 헬기 개발사업의 성공적인 결과로 인하여 노후화된 UH-1및 500MD 헬기를 대체하는 수리온(Surion)에 대한 연구가 활발히 진행되고 있다. 특히, 높은 기동성을 보유한 수리온은 미래 전장에서의 병력수송 및 특수작전 등 다양한 임무를 수행할 것으로 예상되며 이를 지원하기 위한 저고도 전술기동 능력이 요구되고 있다. 그러나 수리온 운용시, 대공 위협 요소를 고려한 최적 저고도 전술기동에 대한 연구는 아직까지 미흡한 실정이다. 본 연구는 강화학습 기반의 알고리즘 중에 하나인 Proximal Policy Optimization(PPO) 알고리즘과 적 대공위협을 고려하여 수리온이 작전 목표지역까지 도달하도록 하는 저고도 상에서의 최적화된 기동 경로를 산출하는 방법론을 제안한다. 이를 위해, Unity 환경과 ML-Agents 라이브러리 상에서 실사화된 수리온 모델을 기초로 약 2×107 회의 강화학습을 진행하였고, 제안하는 방법을 적용하여 수리온의 최단시간 및 최소피해를 달성하는 최적 저고도 전술기동 경로를 산출하는 정책을 도출하였다. 그 결과, '최단 시간' 및 '최소 피해'라는 두 가지 기준을 충족하는 최적 경로가 도출되었다. 본 연구의 결과는 수리온 및 수리온 무인체계를 운용하는 다양한 작전에 활용되어 기동계획을 수립할 시 기동성, 작전성공율, 그리고 생존율을 예측하는데 보탬이 되기를 기대한다.

• International Journal of Control, Automation, and Systems
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• 제1권1호
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• pp.43-53
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• 2003

A modified command shaping control to reduce residual vibrations at a target position and to limit the sway angle of the payload during traveling for container crane systems is investigated. When the maneuvering time is minimized, a large transient amplitude and steady state oscillations may occur inherently. Since a large swing of the payload during the transfer is dangerous, the control objective is to transfer a payload to the desired place as quickly as possible while limiting the swing angle of the payload during the transfer. The conventional shapers have been enhanced by adding one more constraint to limit intermediate sway angles of the payload. The developed method is shown to be more effective than other conventional shapers for prevention of an excessive transient sway. Computer simulation results are provided.

• 한국항공우주학회지
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• 제36권1호
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• pp.31-38
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• 2008

본 논문은 헬리콥터 기동비행문제를 비선형 최적제어기법으로 정식화 하고 이를 indirect method를 적용하여 해석하는 기법에 대한 연구결과이다. 주어진 기동비행 경로에 대한 오차를 벌칙함수 형태의 가격함수로 채택하고 이를 최소화하도록 정식화하면 기동비행은 구속조건이 없는 최적제어문제로 정식화 된다. 정식화 결과로 얻어지는 이점 경계값 문제는 Multiple Shooting Method (MSM)를 적용하여 해석하였다. 본 논문은 high fidelity 헬리콥터 모델링을 적용할 경우 수치해의 불안정성과 과도한 계산시간에 따른 해석의 어려움을 해소하는 방안을 찾는데 초점을 두고 있다. 이를 위해 2가지의 선형모델과 로터의 비선형 모델링을 포함한 2개의 비선형 모델을 정의하였다. 각 모델링 방법의 적용에 따른 수치해석결과를 상대적인 계산시간과 함수계산 횟수 등을 비교하여 헬리콥터 모델 선정 시 활용할 수 있도록 하였다.

• 대한전기학회논문지
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• 제36권12호
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• pp.908-917
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• 1987

Most of moving targets are modelled as nonlinear dynamic equations. In recent years, the extended Kalman filter is frequently used for estimating their behaviors. The conditional Gaussian filter is more suitable than extended kalman filter in the filtering problem of nonlinear systems. But extended Kalman filter and conditional Gaussian filter often do not give optimal estimates and fail to track target trajectories because of its properties. Therefore it is desirable to use adaptive techniques to adapt target maneuvers. In this paper, we will discuss adaptive filtering technique using innovation process based on extended Kalman filter in real time, and suggest another maneuver estimation method using MRAS technique.

• International Journal of Aeronautical and Space Sciences
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• 제13권3호
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• pp.369-376
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• 2012

A nonlinear robust guidance law is designed for missiles against a maneuvering target by incorporating sliding-mode and optimal control theories based on the state dependent Riccati equation (SDRE) to achieve robustness against target accelerations. The guidance law is derived based on three-dimensional nonlinear engagement kinematics and its robustness against disturbances is proved by the second method of Lyapunov. A new switching surface is considered in the sliding-mode control design. The proposed guidance law requires the maximum value of the target maneuver, and therefore opposed to the conventional augmented proportional navigation guidance (APNG) law, complete information about the target maneuver is not necessary, and hence it is simple to implement in practical applications. Considering different types of target maneuvers, several scenario simulations are performed. Simulation results confirm that the proposed guidance law has much better robustness, faster convergence, and smaller final time and control effort in comparison to the sliding-mode guidance (SMG) and APNG laws.

• 한국군사과학기술학회지
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• 제19권5호
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• pp.582-589
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• 2016

Multi-mode monopulse system is widely used for satellite terminal like UAV because of high tracking accuracy and low size/weight profile. In order to calculate tracking error, Multi-mode monopulse system utilizes high-order mode signal, and it should have enough C/N(carrier to noise) level therefore tracking system needs narrow band filtering of received satellite beacon signal as much as possible. However, UAV suffers for beacon frequency drift derived from Doppler effect due to satellite figure 8 movement and UAV maneuvering. Therefore wideband signal processing needs to be considered in advance for exact doppler compensation and consequent time delay. In this paper, we propose the multi-stage Digital Signal processing system for beacon signal, which could minimize the signal delay under high Doppler and low C/N condition.

• International Journal of Naval Architecture and Ocean Engineering
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• 제11권1호
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• pp.606-623
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• 2019

The path following problem of a ship sailing in restricted waters under wind effect is investigated based on Robust $H_{\infty}$ Guaranteed Cost Control (RHGCC). To design the controller, the ship maneuvering motion is modeled as a linear uncertain system with norm-bounded time-varying parametric uncertainty. To counteract the bank and wind effects, the integral of path error is augmented to the original system. Based on the extended linear uncertain system, sufficient conditions for existence of the RHGCC are given. To obtain an optimal robust $H_{\infty}$ guaranteed cost control law, a convex optimization problem with Linear Matrix Inequality (LMI) constraints is formulated, which minimizes the guaranteed cost of the close-loop system and mitigates the effect of external disturbance on the performance output. Numerical simulations have confirmed the effectiveness and robustness of the proposed control strategy for the path following goal of a ship sailing in restricted waters under wind effect.

• 한국군사과학기술학회지
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• 제25권4호
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• pp.401-411
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• 2022

As the role of high-value air assets(e.g., AWACS, JSTARS, Rivet Joint, E-2) becomes more critical in modern warfare, the air escort for these assets blocking attacks from any potential enemy fighter also becomes vital. Without the escort, the operations of the assets become restricted. However, such an escort is not always possible due to the limited flight time of the escort fighters. In this paper, we introduce an escort tactics for high-value air assets performed by the manned-unmanned teaming composed of a transport aircraft and UAVs(unmanned aerial vehicles). In this tactics, the transport aircraft plays the role of an aircraft carrier, which carries, launches, and retrieves the UAVs. The missions of UAVs in this tactics are to detect and engage enemy fighters. We also introduce the simulation result of this tactics to identify the UAVs' required capabilities and optimal maneuvering.