• 한국정밀공학회지
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• 제33권10호
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• pp.781-787
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• 2016

We introduce FEST (Flight Environment Simulation Test) procedures for precise guided missiles to reliably improve systems. Flight vibration specification was established based on power spectral density curves calculated from flight test data of a high speed precise guided missile. A FEST pre-profile was developed according to flight vibration specification and delivered to a precise guided missile assembly. Vibration responses were measured by installing accelerometers on electronic components vulnerable to dynamic forces. The FEST profile was adjusted by comparing the vibration responses and the flight vibration specification. Subsequently, the FEST profile was repeatedly modified through trial and error, because the responses were similar to the flight environment. The modified FEST profile enabled performance testing of assembled precise guided missiles under simulated flight conditions on the ground, where unexpected errors could be corrected before the flight tests, leading to cost and risk reduction in the development of the precise guided missile system.

• 한국군사과학기술학회지
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• 제18권6호
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• pp.816-821
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• 2015

In this paper, an in-flight prediction method of thrust profiles for solid rocket motors is proposed. Actually, it is very difficult to have detailed information about the performance of the rocket motors beforehand because it is quite sensitive to combustion environments. To overcome this problem, we have developed an algorithm for generating in-flight prediction of rocket motor performance in realistic environments via a reference burnback profile and accelerations measured at a short time-interval just after launch. The performance is evaluated through a lot of flight test results.

• 한국추진공학회지
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• 제19권5호
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• pp.98-103
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• 2015

가속도추종 유로개방장치는 고속 비행체의 가압식 연료탱크에서 연료가 쏠림현상으로 인해 단절되는 것을 막아 연속적으로 흐르게 한다. 기개발된 이 유로개방장치를 실제 고속으로 시험하는 것은 까다로운 시험조건과 비용문제로 많은 어려움이 따른다. 따라서 본 논문에서는 저속 항공기에 탑재해 기본적인 역중력 시험(Negative-g test)을 수행하고 RecurDyn으로 해석한 결과와 비교하였다. 그리고 고속비행체의 비행궤적에 따른 유로개방장치의 동역학적 거동을 RecurDyn으로 알아보았다.

• 제어로봇시스템학회논문지
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• 제21권9호
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• pp.888-897
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• 2015

A flight capability to take a terrain following flight near the ground is required to reduce the probability that a fighter aircraft can be detected by foe's radar fence in the battlefield. The success rate for mission flight has increased by adopting TFS (Terrain Following System) to enable the modern advanced fighter to fly safely near the ground at the low altitude. This system has applied to the state-of-the-art fighter and bomber, such as B-1, F-111, F-16 E/F and F-15, since the research begins from 1960's. In this paper, the terrain following system and GCAS (Ground Collision Avoidance System) was developed, based on a digital database with UTAS's TERPRROM (TERrain PROfile Matching) equipment. This system calculates the relative location of the aircraft in the terrain database by using the aircraft status information provided by the radar altimeter and the INS (Inertial Navigation System), based on the digital terrain database loaded previously in the DTC (Data Transfer Cartridge), and figures out terrain features around. And, the system is a manual terrain following system which makes a steering command cue refer to flight path marker, on the HUD (Head Up Display), for vertical acceleration essential for terrain following flight and enables a pilot to follow it. The cue is based on the recognized terrain features and TCH (Target Clearance Height) set by a pilot in advance. The developed terrain following system was verified in the real-time pilot evaluation in FA-50 HQS (Handling Quality Simulator) environment.

• 한국음향학회:학술대회논문집
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• 한국음향학회 1994년도 FIFTH WESTERN PACIFIC REGIONAL ACOUSTICS CONFERENCE SEOUL KOREA
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• pp.710-715
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• 1994

The program name TOLAPS is an acronym for Take-Off LAnding Profile Simulation. Some of the interesting features of this program is the ability to detect flight performance effects of airport altitude, ambient temperature, air pressure and wind. TOLAPS can also handle effects of TOW and LW. The program user can also calculate profiles by user difined flaps and thrust settings deviating from recommended standard settings for each aircraft. Wind effects on straight out flying as well as turns can also be demonstrated. Output form TOLAPS are either screen graphics of profiles (altitude, speed or thrust versus flight distance) or flight track. Profiles can also be made in a tabular form, ready for use in most airport noise calculation programs. In this way, TOLAPS is a valuable tool to evaluate effects of noise abatement procedures.

• 항공우주기술
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• 제7권1호
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• pp.183-193
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• 2008

본 논문은 KSLV-I 상단부에 대한 고장모드 분석 결과와 시스템 수준의 비행시험 신뢰도 모델을 기술한다. 먼저, KSLV-I 상단부의 14개의 주요 기능과 비행시험 임무 프로파일을 분석하고, 기능 분석 결과와 임무 구간별 수행 기능 목록을 바탕으로 시스템 체계에 따른 상단부의 고장모드 계층 구조와 시스템 수준의 비행시험 신뢰도 모델을 구성한다.

• Advances in aircraft and spacecraft science
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• 제8권4호
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• pp.289-302
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• 2021

Ensuring flight safety for passengers as well as crew is the most important aspect of modern aviation, and in order to achieve this, it is necessary to be able to forecast the durability of individual components. The present contribution illustrates the results of a computational analysis to determine the possibility of analysing the prediction of bearing durability in on-board rotating equipment from the point of view of thermal fatigue.In this study, a method developed at the Air Force Institute of Technology was used for analysis, which allowed to determine the bearing durability from the flight altitude profile. Two aircraft have been chosen for analysis - a military M-28 and a civilian Embraer. As a result of the analysis were obtained: the bearing durability in on-board rotating devices, average operation time between failures, as well as failure rate. In conclusion, the practical applicability of this approach is demonstrated by the fact that even with a limited number of flight parameters, it is possible to estimate bearing durability and increase flight safety by regular inspections.

• 한국멀티미디어학회논문지
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• 제25권2호
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• pp.237-246
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• 2022

Among the technologies of the 4th industrial revolution, drones that have grown rapidly and are being used in various industries can be operated by the pilot directly or can be operated automatically through programming. In order to be controlled by a pilot or to operate automatically, it is essential to predict and analyze the optimal path for the drone to move without obstacles. In this paper, after securing and analyzing the pilot training dataset through the unmanned aerial vehicle piloting training platform designed through prior research, the profile of the dataset that should be preceded to search and derive the optimal route of the unmanned aerial vehicle was designed. The drone pilot training data includes the speed, movement distance, and angle of the drone, and the data set is visualized to unify the properties showing the same pattern into one and preprocess the properties showing the outliers. It is expected that the proposed big data-based profile can be used to predict and analyze the optimal movement path of an unmanned aerial vehicle.

• 항공우주기술
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• 제7권1호
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• pp.142-150
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• 2008

KSLV-I 발사체에 탑재되는 원격측정시스템, 추적시스템, 비행종단시템, GPS, 관성항법유도시스템의 개별적인 성능과 고홍우주센터 및 제주추적 소에 설치된 지상장비와의 연계성능을 확인하기 위하여 항공기를 이용한 비행시험이 요구된다. 시험에 적용할 탑재장비의 선정, 하니스, 운용방법, 안테나 부착방법 등의 면밀한 계획과 분석을 통해 시험의 효율성이 향상되기 때문에 KSLV-I의 통신환경과 비행프로파일 둥이 비행시험에 최대한 정확하게 고려되어야 한다. 본 논문에서는 KSLV-I 전자탑재장비의 목록과 규격, 비행시험용 랙과 하니스, 항공기 제원, 비행궤적 둥 효과적인 비행시험을 위해 준비 및 분석되어야 하는 전반적인 사항이 제시된다.

• 한국항공우주학회지
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• 제33권4호
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• pp.91-99
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• 2005

ALQ-X ECM 포드를 KF-16D와 RF-4C 항공기에 장착하기 위한 비행적합성 인증을 수행하였다. MIL-HDBK-1763에 부합하는 외부장착 스토어 인증 절차를 계획한 후 유사성 분석, 기존 스토어 질량 및 관성모멘트 분석, 구조해석 및 시험, 지상진동시험 및 플러터해석을 수행하여 비행시험 수행에 대한 안전성을 확인하였다. ALQ-X 장착 형상을 대표하는 비행 형상으로 MIL-HDBK-1763 Test 250 비행시험을 하였다. ALQ-X 장착 전, 후의 비행특성 차이를 분석하여 조종성을 평가 하고 구조건전성과 내구성은 계측데이터를 함께 분석하여 ALQ-X가 KF-16D 및 RF-4C와 적합성이 있음을 확인하였다. 그 결과로서 ALQ-X를 기존에 인증된 ALQ-88 및 ALQ-119와 동일하게 운용할 수 있음을 인증하였다. ALQ-X 비행인증 결과로서 도입 전투기에 대한 TYPE III 비행적합성 인증, 시험데이터를 사용한 플러터 해석 프로그램을 개발, MIL-STD-1553B 데이터버스를 사용한 비행시험 데이터를 획득할 수 있는 기법과 같은 기술적 성과를 거두었다. 본 비행인증 결과는 향후 국내에서 수행할 Type III 형식의 외부장착 스토어 비행인증의 모델케이스가 될 것으로 기대한다.