• 한국군사과학기술학회지
• /
• 제18권3호
• /
• pp.234-243
• /
• 2015

It is required to have the capability to predict the impact point of the ballistic target in order to assign the firing unit with high engagement possibility for the interception in the ballistic target defense systems. In this paper, a novel method is proposed to predict the impact point of the ballistic target using a flight phase discrimination algorithm given the insufficient measurements on the partial trajectory. The flight of a ballistic target is composed of a boost phase and a ballistic phase with different dynamics. The flight phase is discriminated by using the normalized innovation distance between measurements and a priori estimated measurements. The threshold and tolerance in the flight phase discrimination are determined from the probabilistic characteristics of the estimation error. Monte Carlo simulations are performed to verify the proposed method.

• 한국운동역학회지
• /
• 제28권2호
• /
• pp.69-78
• /
• 2018

Objective: The purpose of this study was to investigate the feasibility of a new vault technique through a kinematic comparison of the YANG Hak Seon and Yeo 2 vaults. Method: The photographic images of the YANG Hak Seon and Yeo 2 vaults were collected using a high-speed camera, and their kinematic characteristics were analyzed using three-dimensional image analysis. Results: During the post-flight phase of the Yeo 2 and YANG Hak Seon vaults, the time of flight, height of flight, and flight distance were similar. At the peak of the post-flight phase, the trunk rotation angle of the YANG Hak Seon vault rotated $457^{\circ}$ more than did the Yeo 2 vault. During the post-flight descending period, the twist velocity of the trunk was much faster with the YANG Hak Seon vault ($1,278^{\circ}/s$) than with the Yeo 2 vault ($1,016^{\circ}/s$). Conclusion: To succeed in the new technique, the average twist velocity during post-flight must be maintained at $1,058^{\circ}/s$ and the twist velocity must be increased from the ascending phase.

• 한국운동역학회지
• /
• 제13권3호
• /
• pp.67-79
• /
• 2003

The purpose of this study is to investigate the effective skill motion through the kinematic analysis of the Yurchenko Streched motion in new horse vaulting. The subjects in this study were 3 male gymnasts who were ranked as national athletes. After the 3D motion analysis, kinematic variables were analyzed to comparison with the difference between this study and the previous study(Yang, D. Y and Lee, C. S, 1999). As a result, the following conclusions was drawn; 1. In the board contact phase, this study showed a shorten contact time to maintain in condition highly extension of hip and hee angle than the previous study. 2. In the pre-flight phase, this study appeared more shortly flight duration time and horizontal flight displacement than the previous study. 3. In the horse contact phase, the contact duration time and horizontal displacement of COG shortened than the previous study, but appeared to the fast horizontal and vertical velocity and highly extension of shoulder an. 4. In the post-flight phase, a stable horse contact appeared to the increase of the flight duration time and the apex height during the post-flight. And it showed that these results have a stable and good landing.

• 한국전자파학회논문지
• /
• 제30권6호
• /
• pp.487-497
• /
• 2019

탄도미사일은 작은 레이다 단면적 및 빠른 기동 특성으로 인하여 탐지가 매우 힘들며, 또한 탄도미사일의 각 비행단계에서 탄두와 유사한 운동 변수로 기동하는 연료탱크 및 기만체의 존재로 인하여 탄두의 식별 및 요격이 매우 어렵다. 따라서 비행 단계에 따라 표적의 기동 및 미세운동을 이용한 특성벡터가 필요하며, 또한 이를 적절히 융합하여 비행단계에 상관없이 식별하는 방법이 요구된다. 본 연구에서는 탄도미사일의 비행단계에 따른 유용한 특성벡터를 소개하고, 이를 특성벡터 및 구분기 레벨에서 융합하는 효과적인 기법을 제안한다. CAD 모델들을 사용하여 예측된 레이다 신호들로 시뮬레이션을 수행한 결과, 구분기 레벨 융합을 통하여 잡음환경 내에서 비행단계에 상관없이 종말 단계로 갈수록 보다 향상된 탄두 식별이 가능하였다.

• 대한금속재료학회지
• /
• 제46권8호
• /
• pp.506-515
• /
• 2008

Recently, it is exceedingly required to produce metal powders with tailored shape and phase altogether in order to fabricate high performance functional parts such as magnetic core or electro-magnetic noise suppressor for high frequency usage. Therefore, the collision phenomena of in-flight droplets against chamber wall or neighboring in-flight droplets each other is investigated by a computational method in order to get useful information about how to design the atomizing system and how to tailor process parameters not to make irregular-shaped powders during gas atomization process. As a results, smaller powders, lower melt temperature are known to be favorable for droplets not to collide against chamber wall. In additions, powders of narrower size distribution range, lower droplet generation rate, lower melt temperature, lower gas velocity are desirable to prevent droplet-collisions against neighboring in-flight droplets.

• 전자공학회논문지SC
• /
• 제40권4호
• /
• pp.291-298
• /
• 2003

질병을 진단하기 위하여 환부를 가시화하는 것은 매우 중요하다. 많은 경우 환부의 형태학적 변화를 동반하기 때문이다. 혈관에서의 이러한 형태학적 특성을 가시화하는 기법을 혈관 조영기법 이라 한다. 혈관조영기법은 TOF 기법과 위상대조도 기법, 조영제 증강 기법이 있다. 본 논문에서는 혈관 조영기법에 대한 각각의 원리와 관련된 시퀸스 및 특성에 대하여 소개하고 촬영을 통한 데이터 획득후의 데이터 후처리의 과정을 기술하였으며 인체에 응용의 최근 사례들을 소개하였다.

• 한국건축시공학회지
• /
• 제23권3호
• /
• pp.327-336
• /
• 2023

The focus of this research was to devise a conceptual methodology for drone usage and to assess the viability of safety checklist items specific to drone application in safety oversight. The appraisal was grounded in a focus group interview involving professionals from construction management and safety fields. The proposed process was segmented into four stages: 1) pre-flight phase for flight plan development, 2) drone flight phase for safety condition inspection utilizing checklist items, 3) post-flight phase for visual asset analysis, and 4) documentation and management phase. Furthermore, the research scrutinized the applicability of 32 distinct safety checklist items for drone operations. The primary aim of this investigation was to probe the possible deployment of drones as part of construction safety inspections at work sites. However, it bears mentioning that subsequent research should strive to gather a more extensive sample size through questionnaire surveys, thereby facilitating quantitative analysis. Administering such surveys would yield more comprehensive data compared to a focus group interview, which was constrained by a limited participant count. In summation, this study lays a foundational groundwork for understanding the potential advantages and challenges associated with integrating drones into construction safety management.

• International Journal of Aeronautical and Space Sciences
• /
• 제13권3호
• /
• pp.267-281
• /
• 2012

This paper reviews the flight mechanics and control of birds and bird-size aircraft. It is intended to fill a niche in the current survey literature which focuses primarily on the aerodynamics, flight dynamics and control of insect scale flight. We review the flight mechanics from first principles and summarize some recent results on the stability and control of birds and bird-scale aircraft. Birds spend a considerable portion of their flight in the gliding (i.e., non-flapping) phase. Therefore, we also review the stability and control of gliding flight, and particularly those aspects which are derived from the unique control features of birds.

• 한국군사과학기술학회지
• /
• 제16권3호
• /
• pp.268-276
• /
• 2013

The objective of this paper is to give a general understanding for the development flight test of Korean Utility Helicopter(KUH). This paper contains the contents of detailed flight test plan, the type of flight test, an introduction to main flight test area, and the overview of flight test results. At the beginning, more than 8,500 test points were identified for airworthiness certification to show the compliance for the KUH development requirements. However, the number of flight test points were optimized to 7,800 at the end. To accomplish the test objectives, about 860 flight test sorties had been performed, and more than 1,000 test sorties were consumed for trouble shooting. This paper also describes some major issues faced during development flight test phase.

• 한국항공운항학회지
• /
• 제17권1호
• /
• pp.52-57
• /
• 2009

One of the error sources for microwave ranging is the instability of the oscillator that drives the microwave signals. Dual one-way ranging (DOWR) minimizes the oscillator effect by combining two one-way carrier phase signals from two transmitter/receiver instrument. The DOWR is first implemented in the GRACE (Gravity Recovery and Climate Experiment) satellites. Direct evaluation of the DOWR is not possible due to its extremely high accuracy. The flight performance of the GRACE DOWR is analyzed by applying several indirect methods. Comparison with the design noise level is discussed.