• International Journal of Aeronautical and Space Sciences
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• 제18권1호
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• pp.154-164
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• 2017

This work conducts a validation study for the XH-59A helicopter using a rigid coaxial rotor system in order to establish the techniques of the conceptual design and performance analysis for the lift-offset compound rotorcraft. As a tool for conceptual design and performance analysis, NDARC (NASA Design and Analysis of Rotorcraft) is used for the present study. An assumed mission profile is considered for the conceptual design of the XH-59A. As a validation result of the design, the dimensions and weight of the XH-59A are appropriately designed when compared to the target values since the relative error is less than 0.5%. Then, performance analyses are conducted for the designed XH-59A model with and without auxiliary propulsion in hover and forward flight conditions. The present analyses show good validity since the prediction results compare well with both the flight test and previous analyses. Therefore, the techniques for the conceptual design and performance analysis of the lift-offset compound helicopter are overall considered to be appropriately established. In addition, this study investigates the influence of the lift-offset on the rotor effective lift-to-drag ratio of the XH-59A helicopter with auxiliary propulsion. As a result, the improvement of the rotor effective lift-to-drag ratio can be obtained by appropriately increasing the lift-offset in high-speed flight.

• 한국군사과학기술학회지
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• 제17권3호
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• pp.304-310
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• 2014

Based on atmosphere weather data by balloon in Osan and Gwangju area, if icing condition occurs in weather environment of altitude range where helicopter is operated was analyzed in quantitative way. Yearly icing occurrence frequency for daytime during recent three years was average 102 days in Osan, average 91 days in Gwangju. Icing weather environment to highly affect operation of helicopter varies a little according to analysis methods but icing intensity at MDT level was calculated in all the methods, and 14.5~38 times was suggested in Osan; 2.5~30 times in Gwangju. Icing at MDT level was calculated in common in all the analysis methods through wide periods such as Jan., Feb., Mar., and Nov. in Osan. In Gwangju, icing at MDT level was suggested focusing on Jan. only. Therefore, military helicopter developed in Korea is required to strive obtaining certificate of airworthiness about icing condition at MDT level for implementation of perfect operational mission and safe operation.

• 산업경영시스템학회지
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• 제43권4호
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• pp.150-160
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• 2020

In this paper, we introduce a pilot's scheduling model which is able to maintain and balance their capabilities for each relevant skill level in military helicopter squadron. Flight scheduler has to consider many factors related pilot's flight information and spends a lot of times and efforts for flight planning without scientific process depending on his/her own capability and experience. This model reflected overall characteristics that include pilot's progression by basis monthly and cumulative flight hours, operational recent flight data and quickly find out a pinpoint areas of concern with respect to their mission subjects etc. There also include essential several constraints, such as personnel qualifications, and Army helicopter training policy's constraints such as regulations and guidelines. We presented binary Integer Programming (IP) mathematical formulation for optimization and demonstrated its effectiveness by comparisons of real schedule versus model's solution to several cases experimental scenarios and greedy random simulation model. The model made the schedule in less than 30 minutes, including the data preprocessing process, and the results of the allocation were more equal than the actual one. This makes it possible to reduce the workload of the scheduler and effectively manages the pilot's skills. We expect to set up and improve better flight planning and combat readiness in Korea Army aviation.

• 한국전자파학회:학술대회논문집
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• 한국전자파학회 2005년도 종합학술발표회 논문집 Vol.15 No.1
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• pp.23-28
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• 2005

An airborne radar is an essential aviation electronic system of the helicopter to perform various missions in all-weather environments. This paper presents the results of the design and implementation of the airborne pulse doppler radar signal processor using high multi-DSP for the multi-function radar capability such as short-range, midium-range, and long-range depending on the mission of the vehicle. Particularly, the radar signal processor is developed using two DSP boards in parallel for the various radar signal processing algorithm. The key algorithms include LFM chirp waveform-based pulse compression, MTI clutter filter, MTD processor, adaptive CFAR, and clutter map. Especially airborne moving clutter Doppler spectrum compensation algorithm such as TACCAR is implemented for the multi-mode airborne radar system. The test results shows the good Doppler spectral separation for the clutter and the moving target in the flight test environment using helicopter.

• 한국군사과학기술학회지
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• 제14권4호
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• pp.598-606
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• 2011

The importance of avionics systems has increased to a significant level in modern aircraft development. Modern avionics system is a complex integrated system of state-of-art hardware and software technology. Specifying the avionics system architecture is the most important task throughout the avionics system design process. This paper reviews modern avionics system architectures and proposes an effective avionics architecture suitable for modern attack helicopters.

• 항공우주시스템공학회지
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• 제15권6호
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• pp.72-77
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• 2021

This paper proposes a design and development plan for a control program for the MX-10 EO/IR camera. This camera is a piece of mission equipment mounted on the multi-purpose unmanned helicopter (MPUH) system. Operators must be able to control the necessary functions of the camera to perform their assigned tasks. To achieve this, the function to control the camera was analyzed, and a control program was developed. In addition, the control program was linked to a joystick for convenient operation of the camera by the operator.

• 한국정보통신학회논문지
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• 제22권2호
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• pp.354-361
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• 2018

본 논문은 비행제어 비행체 관리 시스템 대신 한국형 기동헬기 임무컴퓨터의 비행운용 프로그램에서 구현한 측면 항법 알고리즘 설계 및 검증에 대하여 기술하였다. 구현된 측면항법 기능은 비행제어 시스템으로 롤 명령을 보내고 롤 명령 값은 임무컴퓨터의 제어 알고리즘에서 계산한다. 임무컴퓨터에서 제어 알고리즘 계산 시 항공기의 자세 및 위치에 대한 측정값을 이용한다. 이 입력 값들을 이용하여 임무컴퓨터에 탑재된 비행운용 프로그램은(선택한 비행계획 등)항법 요구를 롤 명령으로 자동조종으로 보낸다. 체계통합리그에서의 통합시험, 지상 및 비행시험을 통해 측면 항법 알고리즘을 검증하였다.

• 대한전자공학회:학술대회논문집
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• 대한전자공학회 2005년도 추계종합학술대회
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• pp.443-446
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• 2005

This paper presents the results of the design and implementation of the airborne pulse doppler radar signal processor using high multi-DSP for the multi-function radar capability such as short-range, midium-range, and long-range depending on the mission of the vehicle. Particularly, the radar signal processor is developed using two DSP boards in parallel for the various radar signal processing algorithm. The key algorithms include LFM chirp waveform-based pulse compression, MTI clutter filter, MTD processor, adaptive CFAR, and clutter map. Especially airborne moving clutter Doppler spectrum compensation algorithm such as TACCAR is implemented for the multi-mode airborne radar system. The test results shows the good Doppler spectral separation for the clutter and the moving target in the flight test environment using helicopter

• 항공우주기술
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• 제5권2호
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• pp.1-7
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• 2006

본 논문에서는 무인헬기에 적합한 새로운 형태의 점항법 유도법칙을 소개한다. 본 점항법 유도법칙은 미래의 예측 위치에 기반하여 자동제어부에서 사용할 속도와 방위각 명령을 생성해낸다. 무인기의 뱅크각을 통해 간접적으로 비행방향을 변경하는 기존의 점항법 유도법칙과 달리 본 유도법칙은 무인헬기의 속도벡터를 직접 변경하도록 속도 명령을 생성해낸다. 제안된 유도법칙의 검증을 위해 소형 무인헬기용 비행제어시스템을 개발해 비행 시험을 수행하였으며, 개발된 비행제어시스템은 비행제어 컴퓨터와 항법센서, 그리고 지상관제국으로 구성되어 있다. 비행시험을 통해 제안된 유도법칙이 성공적으로 작동함을 확인하였으며, 향후 경로추종 비행에 확장.적용할 계획이다.

• 한국항공우주학회지
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• 제40권7호
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• pp.623-628
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• 2012

임무탑재장비 체계는 한국형 기동헬기의 임무 수행을 위해 전자장비 구성품들을 통합한 항공전자 체계다. 자체진단 시험은 숙련된 요원, 특수 시험장비의 필요성을 감소시키주며 체계의 정비를 위한 비가동 시간을 줄여준다. 갈수록 복잡성이 증가하고 있는 항공전자 장비에 대한 자체진단 시험 기능의 필요성이 더욱 커지고 있다. 본 논문은 한국형 기동헬기 항공전자 체계에 구현한 자체진단 시험 설계 및 입증에 대해 설명한다.