• Title/Summary/Keyword: 초기트림

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Helicopter Trim Analysis and Flight Simulation by Uising DAE Based PPTA (Partial Periodic Trimming Algorithm) (DAE 해법과 PPTA(Partial Periodic Trimming Algorithm)를 이용한 헬리콥터 트림해석 및 비행 시뮬레이션)

  • Kim,Chang-Ju
    • Journal of the Korean Society for Aeronautical & Space Sciences
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    • v.31 no.1
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    • pp.42-48
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    • 2003
  • To get a periodic trim solution from Level II helicopter flight dynamic equations, DAE based PPT A (partial Periodic Trimming Algorithm) has been proposed. Iterative update of state variables from PPT A can cause a numerical instability in DAE solver which needs compatible initial conditions. By simply adjusting the order of DAE solver a periodic trim can be obtained with good accuracy. Application for CBM (Common Baseline Model) helicopter showed the same trim result as harmonic balance method and the effective elimination of unrealistic initial responses at the start of flight simulation.

An Experimental Study on the Resistance Performance of Small Size Fishing Vessel (소형 연안어선의 저항성능에 관한 실험적 연구)

  • Kim, Do-Jung;Park, Je-Woong;Kim, Ju-Nam;Jeong, Uh-Cheul
    • Journal of the Korean Society of Fisheries and Ocean Technology
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    • v.40 no.4
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    • pp.304-310
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    • 2004
  • Resistance performance of small size fishing vessel is experimentally investigated to find out the effect of fore-body shape and trim for the better hull from development. The tests are performed for five different cases in the high speed circulating water channel(CWC). Wave patterns are observed to investigate the relation between the resistance performance and the wave characteristics.

Sensor Fault Detection for Small Turboshaft Engine Considering Multiple Trim Conditions (다중 트림 상태를 고려한 소형 터보샤프트 엔진의 센서 고장 검출)

  • Seong, Sang-Man;Rhee, Ihn-Seok;Ryu, Hyeok
    • Proceedings of the Korean Society of Propulsion Engineers Conference
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    • 2008.11a
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    • pp.192-195
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    • 2008
  • A sensor fault detection method for small turbo shaft engine considering multiple trim conditions is proposed. This engine is used in a helicopter. Firstly, under multiple trim conditions, we derive the linearized models from a nonlinear model which includes engine, rotor and feedback control loop. As a fault detection method, we adopt the Kalman filter based method. To keep continuity of estimates between the changes of trim conditions, we reconfigure the initial values of state variables at trim changes. We detect the faults with two steps that when the first filter does not alarm the faults for some sensors, the second filter is runned for other sensor. Via some simulations we show that the proposed method works well under multiple trim conditions.

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Study on durability test method for improvement of door trim grip handle friction noise (도어트림 그립핸들 마찰이음 근본개선을 위한 내구 시험법 개발 및 개선연구)

  • Kim, Jongsoo;Na, Hyunghyun;Cho, Youngbin
    • The Journal of the Acoustical Society of Korea
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    • v.37 no.4
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    • pp.233-241
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    • 2018
  • In this paper, we develop a durability test method that can verify the noise caused by the repeated load on the door trim grip handle. The test method was developed in consideration of the load mode and durability test cycle applied to the grip handle. In order to verify the validity of the method, we demonstrated the door trim grip handle noise that occurred in the field claim with the product in the early stage of mass production through the developed test method. Finally, It is used to detect and improve the noise of subsequent development products through the currently developed test method.

Study on the Stability Estimation Method of Small Fishing Vessels at the Initial Design Step (초기설계 단계에서 소형 어선의 복원성 추정 방안에 관한 연구)

  • Hwe-Woo Kim;Sanghyun Kim;Sun-Woo Lee;Hyogeun Lee;In-Tae Kim
    • Journal of the Korean Society of Marine Environment & Safety
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    • v.29 no.7
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    • pp.863-870
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    • 2023
  • Ship capsize accidents are common in coastal waters, particularly involving small fishing boats. To prevent there overturing accidents in small fishing boats, their stabilities must be assessed at the initial design step. However, the available information during the initial design step is limited, posing challenges in performing a reliable stability evaluation. Therefore, this study presents a plan to estimate the transverse metacenter (GM) of small fishing boats using parameters such as KM, KG, and TRIM that can be determined at the initial design step. Stability was evaluated by comparing GM with the minimum transverse metacenter (GMmin) specified in the standard safety evaluation criteria for fishing boats. To calculate the required trim value for hydrostatic characteristics using K-SHIP, a stability assessment program provided by the Korea Maritime Safety and Transportation Corporation, the initial trim state is estimated based on the ship lines using the commercial CFD program STAR-CCM+. GM is then calculated by assessing the hydrostatic characteristics in relation to the boat lines using K-SHIP. Furthermore, the stability of the fully loaded state is compared by subtrcating GM from GMmin. One constructed ship is designated as the standard ship, and the stability assessment method proposed in this study is applied to evaluate stability and validate its effectiveness. Consequently, the representative line of a 4.99-ton fishing boat and nine modular lines models derived from it were evaluated, ultimately identifying a relatively superior stability.

A Study on Improvement of Roll Autopilot System (가로축 자동비행시스템 개선에 관한 연구)

  • Kim, Chong-Sup;Koh, Gi-Oak;Ji, Chang-Ho;Cho, In-Je;Lee, Dong-Kyu
    • Journal of the Korean Society for Aeronautical & Space Sciences
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    • v.43 no.8
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    • pp.706-711
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    • 2015
  • The fighter aircraft uses several different loading configurations for air-to-surface and air-to-air combat missions. To maintain wings-level flight with an asymmetric weapon configuration, a pilot controls a roll trim system. However, it is difficult to apply an accurate roll trim input for wings-level flight in the actual flight under disturbance. The inaccurate roll trim input degrades the performance of the roll autopilot system. In this paper, to solve this problem, an integrator was additionally designed in the command part of the roll autopilot system. The initial transient response was improved by scheduling the limiter to restrict the roll attitude error. As a result of the evaluation of the simulation for the designed flight control law, the roll attitude following performance was found to be improved in the autopilot system operation under the inaccurate roll trim condition.

A Study on the Initial Hull Form Development and Resistance Performance of a 45 Knots Class High-Speed Craft (45노트급 고속정의 초기선형 개발과 저항성능에 관한 연구)

  • KIM JU-NAM;JEONG UH-CHEUL;PARK JE-WOONG;KIM DO-JUNG
    • Journal of Ocean Engineering and Technology
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    • v.20 no.1 s.68
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    • pp.32-36
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    • 2006
  • The initial hull form of a 100 tan, 45 knot class high-speed craft is newly developed. The resistance performances are investigated using a model test at high speed in a circulating water channel. The effect of the initial trim is studied together. Wave patterns are observed to clarify the relationship between the resistance performance and the wave characteristics. It can be found that the initial trim plays a role in increasing the resistance performance above a certain velocity.

Improved Fast Correlation Attack on the Shrinking and Self-Shrinking generators (Shrinking 생성기와 Self-Shrinking 생성기에 대한 향상된 고속 상관 공격)

  • Jeong Ki-Tae;Sung Jae-Chul;Lee Sang-Jin;Kim Jae-Heon;Park Sang-Woo;Hong Seok-Hie
    • Journal of the Korea Institute of Information Security & Cryptology
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    • v.16 no.2
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    • pp.25-32
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    • 2006
  • In this paper, we propose a fast correlation attack on the shrinking and self-shrinking generator. This attack is an improved algorithm or the fast correlation attack by Zhang et al. at CT-RSA 2005. For the shrinking generator, we recover the initial state of generating LFSR whose length is 61 with $2^{15.43}$ keystream bits, the computational complexity of $2^{56.3314}$ and success probability 99.9%. We also recover the initial state of generating LFSR whose length is $2^{40}$ of the self-shrinking generator with $2^{45.89}$ keystream bits, the computational complexity of $2^{112.424}$ and success probability 99.9%.

A Study on the Hull Form Development and Resistance Performance of a High-Speed Coastal Patrol Boat (고속 연안순시선 선형개발과 저항성능에 관한 연구)

  • 정우철;정석호;전호환
    • Journal of Ocean Engineering and Technology
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    • v.18 no.3
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    • pp.44-49
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    • 2004
  • Initial hull form of 10 G/T and 40 knots class coastal patrol boat is newly developed. The resistance performances are experimentally and numerically investigated by model test and CFD technique. The effect of initial trim and a fin attached at hull side are studied together. Wave patterns are observed to make clear the relation between the performance and the wave characteristics. It can be found that the initial trim plays a role in increasing the resistance performance above a certain velocity, and the CFD technique can be used at the initial design stage of a high-speed planning boats.

The Related-Key Attack on Grain-v1 (스트림 암호 Grain-v1에 대한 연관키 공격)

  • Lee, Yu-Seop;Jung, Ki-Tae;Sung, Jae-Chul;Hong, Seok-Hie
    • Journal of the Korea Institute of Information Security & Cryptology
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    • v.18 no.4
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    • pp.45-52
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    • 2008
  • The slide resynchronization attack on Grain-v1 was proposed in [5]. Given the keystream sequence, this attack can generate the 1-bit shifted keystream sequence generated by Grain-v1. In this paper, extending the attack proposed in [5], we propose the key recovery attack on Grain-v1 using the related-key. Using the weakness of the initialization procedure of Grain-v1, this attack recover the master key with $2^{25.02}$ Ⅳs and $2^{56}$ time complexity. This attack is the first known key recovery attack on Grain-v1.