• Proceedings of the Korean Society of Propulsion Engineers Conference
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• 2007.11a
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• pp.267-270
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• 2007

Korea Aerospace Research Institute(KARI) made a scramjet engine test contract with the University of Queensland in October 2006. The experiments were conducted at Mach 7.6, Altitude 31.2 km condition in the T4 free piston-driven shock tunnel in June 2007. In this paper, the short introduction and data processing technique of the T4 free piston-driven shock tunnel will be explained.

• Proceedings of the Korean Information Science Society Conference
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• 2010.06b
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• pp.28-33
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• 2010

최근 모바일 게임에 있어서 중요한 이슈는 게임상에서 존재하는 물체들이 사실감과 생동감을 유지하면서도 프로그램의 속도 감소 문제를 발생시키지 않는 방안을 찾는 것이다. 본 논문이 제시하는 내용은 모바일 환경에서의 지능형 물리엔진 아키텍쳐에 대한 것으로 물리엔진으로 구현 한 게임 안의 환경을 인지하고 수집한 수치를 이용, 학습하여 사용자가 컨트롤하는 게임 내의 물체가 최적화 된 움직임을 보일 수 있도록 하는 데 목표를 두고 있다. 이를 위해 모바일 환경에 적합하도록 구현된 물리엔진으로 자동차 주행 시스템 환경 내에서 속성을 추출, 인공지능 모듈에 입력하여 연산량이 비교적 적은 베이지안 네트워크 알고리즘을 통해 분석하며 이를 평가한다.

• Journal of Korea Game Society
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• v.15 no.6
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• pp.97-106
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• 2015

In an Unity engine for multi-player online games, the main thread processing game logic must be separated from the network thread that is responsible for network packet communication. Packet communication between the network threads needs to drop packets that overlap in order to improve the rendering speed. In this paper, the packet discard policy of network thread is proposed for an Unity engine for multi-player online games. The proposed method is the hybrid method of both Partial Packet Discard and Periodic Packet Discard methods to improve the rendering speed by periodically discarding overlapped network packets managed by the queue. The rendering speed of the proposed method is analyzed and its effectiveness is verified by various packet generating simulations of the Unity engine for multi-player online games.

• Proceedings of the Korean Society of Propulsion Engineers Conference
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• 2009.11a
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• pp.125-129
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• 2009

The basic design of liquid rocket engine combustion chamber for a large space launch vehicle was described. It has vacuum thrust of 74.8 ton, vacuum specific impulse of 306.9 sec, chamber pressure of 60 bar, mass flow rate of 243.6 kg/s and combustion characteristic velocity of 1730 m/sec. The details of combustion performance and geometrical parameter were also given. The 75 ton combustion chamber consists of the combustor head with injector and the chamber/nozzle with regenerative cooling channels.

• Proceedings of the Korean Society of Propulsion Engineers Conference
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• 1998.04a
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• pp.5-5
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• 1998

가스터빈 엔진은 민간 항공분야와 방위 무기의 발달과 더불어 성능이 향상되어 왔고, 그 역할도 증대하였다. 성능 향상과 역할 증대에 따라 처리하여야 할 일의 양과 그 속도가 증가하게 되면서 엔진 제어 난이도도 증가하고 제어기법도 향상되고 있다. 이에, 전자공학의 발달에 힘입어 전자식 엔진 제어기가 엔진제어의 임무를 수행하게 되었고, 근래에는 기체의 무게감소와 신뢰성 향상이라는 이중 이익을 위해 FADEC(Full Authority Digital Engine Controller)엔진 제어기까지 등장, 사용되고 있다. 가스터빈 엔진의 제어는 일반적으로 비선형 시스템에 관한 모델링 단계와 성능 해석결과를 이용한 보상기 설계 및 제어 단계의 3부분으로 크게 분류된다. FADEC이란 개념이 정착되기 이전에는 통상적인 제어 법칙인 PID(Proportional Integral Derivative) 방법이 사용되었으나, 시스템의 복잡화와 다변화에 의하여 modern control 개념이 고려된 새로운 제어 방법이 사용되기 시작하였다. 본 논문에서는 엔진 제어에 실제적으로 이용할 수 있는 제안된 제어 법칙을 이용하여 실제 엔진 모델에 적용하여 시뮬레이션 함으로써 새로운 제어 법칙이 엔진 제어에 적용 가능함을 보이고자 한다.

• The Journal of the Acoustical Society of Korea
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• v.40 no.6
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• pp.571-577
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• 2021

This study is a study on System On Chip (SOC) that implements virtual engine sound in electric vehicles without engines, and realizes vivid engine sound by combining Adaptive Difference PCM (ADPCM) method and frequency modulation method for satisfaction of driver's needs and safety of pedestrians. In addition, by proposing an electronic sound synthesis algorithm applying Musical Instrument Didital Interface (MIDI), an engine sound synthesis method and a constitutive model of an engine sound generation system are presented. In order to satisfy both drivers and pedestrians, this study uses Controller Area Network (CAN) communication to receive information such as Revolution Per Minute (RPM), vehicle speed, accelerator pedal depressed amount, torque, etc., transmitted according to the driver's driving habits, and then modulates the frequency according to the appropriate preset parameters We implemented an interaction algorithm that accurately reflects the intention of the system and driver by using interpolation for the system, ADPCM algorithm for reducing the amount of information, and MIDI format information for making engine sound easier.

• Journal of the Korea Academia-Industrial cooperation Society
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• v.19 no.11
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• pp.529-535
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• 2018

The range extender vehicle runs on a mechanism that allows the small power generation engine to start in the most efficient specific operating range to charge the battery and extend the mileage. In this study, we developed a step motor type intake air supply system that replaces existing throttle body system to develop a simple low cost control logic system. The system was applied to the existing base engine, and in order to improve the performance by increasing the amount of intake air, the effect of changing the length of the intake and exhaust manifold was experimentally examined. As a result, the Type B intake air control actuator operated by one step motor showed higher performance than the Type A in all the operation region, but the performance was lower than that of the base engine due to the increase of flow resistance. To improve this, it was confirmed that the engine performance was improved at both speeds of 2200rpm and 4300rpm when the 140mm adapter was installed in the intake manifold and when the newly designed 70mm exhaust manifold was applied. Through this process, high - precision operation control was realized by connecting the generator load to the optimized engine for the range extender electric vehicle. Experimental results showed that the speed change rate was within ${\pm}2.5%$ at 2200rpm in 1st stage and 4300rpm in 2nd stage and the speed follow-up result of 610 rpm/s was obtained when the speed was increased from 2200rpm to 4300rpm.

• Journal of the Institute of Electronics Engineers of Korea SD
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• v.46 no.6
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• pp.39-47
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• 2009

This paper presents implementation of two types of the 802.11 MAC engine for the next generation WLAN, 802.11n. The first version of MAC engine consists of hardwired logic and embedded firmware. Hardwired logic includes Tx block, Rx block, Backoff block, and ChannelManage block. Embedded firmware contains Protocol Control block, MLME block, and MSDU processing block. The first version has a time-critical fault during the atomic transmission caused by software overhead, so it can not be applied to 802.11n MAC. For that reason, the second version has additional blocks with hardwired logic modules to reduce software overhead of the first version. This enhanced version has 73Mbps throughput and it is expected to be further improved up to 129 Mbps with frame aggregation which is one of the key additional features of 802.11n. As a result, the second version of MAC engine can be applied to 802.11n MAC.

• Journal of Advanced Navigation Technology
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• v.10 no.4
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• pp.319-326
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• 2006

In this paper, a fuzzy inference control system is proposed for a turbojet engine with fuel flow control input only. The proposed control system provides a practical fuel flow control method to prevent surge or flame out during engine acceleration or deceleration. A fuzzy logic is designed to obtain the fast acceleration and deceleration of the engine under the condition that the operating point should stay between the surge line and flame out control line. With using both engine rotating speed error and surge margin as fuzzy input variables, the desired engine rotating speed can be achieved to rapidly follow the engine control line without engine stall. Computer simulation using the MATLAB is realized to prove the proposed control performance to the turbojet engine which is linear modelized using DYGABCD program package.

• Transactions of the Korean Society of Mechanical Engineers
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• v.17 no.6
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• pp.1633-1639
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• 1993

In spark ignition engine, EGR of lean mixture operation has advantage in emission, but disadvantages in power output and combustion flame propagation. Fast burn system is known to be a useful method to solve these disadvantages. This paper presents the characteristics of in-cylinder flow for different combustion chamber geometries, and the correlation between the in-cylinder flow and the combustion flame speed using an ion current method.