• 제목/요약/키워드: Unmanned agricultural machinery

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Utilization of Laser Range Measurements for Guiding Unmanned Agricultural Machinery

  • Jung, I. G.;Park, W. P.;Kim, S. C.;Sung, J. H.;Chung, S. O.
    • Agricultural and Biosystems Engineering
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    • 제2권2호
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    • pp.69-74
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    • 2001
  • Detection of operation lines in farm works, object recognition and obstacle avoidance are essential pre-requisite technologies for unmanned agricultural machinery. A CCD camera, which has been largely used for these functions, is expensive and has difficulty in real-time signal processing. In this study, a laser range sensor was selected as the guiding vision for unmanned agricultural machinery such as a tractor. To achieve this capability, algorithms for distance measurement, signal filtering, object recognition, and obstacle avoidance were developed. Computer simulations were carried out to evaluate performance of the algorithms. Experiments were also conducted with various materials and shapes, Laser beam lost its intensity for poor reflective materials, resulting in less range value than actual, so a compensation technique was considered to be necessary. Object detection system was fabricated on an agricultural tractor and the performance was evaluated. As test result for obstacle detection and avoidance in field, to detect and avoid obstacle for path finding with guiding system for unmanned agricultural machinery was enable.

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소형 무인헬기를 이용한 항공방제기술 (I) - 현황 및 경제성 분석 - (Aerial Application using a Small RF Controlled Helicopter (I) - Status and Cost Analysis -)

  • 구영모;이채식;석태수;신시균;강태경;김승희;최태영
    • Journal of Biosystems Engineering
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    • 제31권2호
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    • pp.95-101
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    • 2006
  • Present chemical application system using a power sprayer has been a labor intensive, ineffective and shirking task in farming. Therefore, a small RF controlled (unmanned) helicopter was suggested to replace the conventional spray system. The aerial application using the unmanned helicopter has been already utilized in Japan, where total area applied up to 704,000 ha in 2005. In this article, the status and cost analysis on the unmanned agricultural helicopter were studied. The aerial application using the agricultural helicopter helps precise and timely spraying and reduces labor intensity and pollution. The field capacity of the helicopter was found to be 60-70 ha a day. The break even point was estimated near the operating area of 750 ha annum. The development of an agricultural helicopter was necessary for taking advantages of both technique and economy.

무인 곡물 수확기 지능수준 등급구분에 관한 연구 (A Research on the Classification of Intelligence Level of Unmanned Grain Harvester)

  • 조나;반영환
    • 한국융합학회논문지
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    • 제11권5호
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    • pp.165-173
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    • 2020
  • 무인 농기계의 출현으로 정밀 농업의 발전에 새로운 연구 콘텐츠가 등장했다. 무인 농기계의 핵심 기술 연구를 가속화시키기 위해 먼저 무인 농기계 지능 수준 분류가 일 차적 과제가 되어 왔다. 이에 본 연구는 무인 곡물 수확기, 작업, 운전 환경으로 구성된 복합 양방향 시스템을 연구 대상으로 하고, 무인 곡물 수확기의 지능화 수준을 등급화하고 분류하는 연구를 수행한다. 본 연구의 연구자들은 인적 개입 정도, 환경적 복잡성, 작업 복잡성으로 구성된 무인 곡물 수확기 차량의 평가 모델을 확립한다. 또한, 무인 곡물 수확기의 지능화 수준 등급화와 분류는 인적 개입 정도, 환경적 복잡성과 작업 난이도에 따라 이루어진다. 무인 농기계의 미래 발전 방향을 제시하고 있다.

저투입 소필지 정밀 살포용 무인헬리콥터의 기체개발 - 기체요소의 개념설계 및 시작기 - (Mechanical Development of an Unmanned Helicopter for Precise Small-scaled ULV Aerial Application - Conceptual Design and Prototype -)

  • 구영모;석태수;신시균;이채식;강태경
    • Journal of Biosystems Engineering
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    • 제33권2호
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    • pp.94-100
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    • 2008
  • Present chemical application method using a power sprayer has been labor intensive, costly and ineffective. Therefore, a small agricultural unmanned helicopter was suggested to replace the conventional spray system. In this study, conceptual design for developing the helicopter and a consequential prototype were reported. The overall conceptual design was initiated by deciding the type of agricultural helicopter, as the single rotor helicopter with a tail system. As the first step of the designing, an air-cooled, 2-stroke engine was selected and a prototype transmission was designed by determining the rotating speed of main rotor shaft. A 'pusher' type tail rotor system was adapted to balance the reaction torque and reduce the power use. The tail boom length was designed to avoid the rotating trajectory of the main rotor. The RF console consisted of the engine control, attitude control, and emergency control modules. Assembling the prototype concluded the mechanical development of the agricultural helicopter.

농용 무인헬리콥터의 가로균평을 위한 테일부 설계 및 추력 시험 (Tail Rotor Design and Thrust Test for a Roll-balanced Agricultural Unmanned Helicopter)

  • 구영모;배영환;석태수;신시균;박희진
    • Journal of Biosystems Engineering
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    • 제35권5호
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    • pp.302-309
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    • 2010
  • Aerial application using an unmanned agricultural helicopter would allow precise and timely spraying. The attitude of a helicopter depends on a number of dynamic variables for roll-balanced flight. Laterally tilting behavior of a helicopter is a physically intrinsic phenomenon while hovering and forwarding. In order to balance the fuselage, the rotor should be counter-tilted, resulting in the biased down-wash. The biased spraying toward right side causes uneven spray pattern. In this study, a raised tail rotor system for the roll-balanced helicopter was studied. Thrust of the tail rotor system was measured and theoretically estimated for the fundamental database of the roll-balanced helicopter design. The estimated tail thrust and roll-moment would be used to design the raising height of tail rotor and roll balancing dynamics. The unmanned agricultural helicopter required the tail rotor thrust of about 39.2 N (4.0 kgf) during hovering with a payload of 235.4 N (24 kgf). A raised tail rotor system would compensate for the physical tilt phenomena. A further attitude control system of helicopter would assist roll-balanced aerial spray application.

소형 무인헬기를 이용한 항공방제기술 (III) - 로터부의 양력시험 - (Aerial Application Using a Small RF Controlled Helicopter (III) - Lift Test of Rotor System -)

  • 구영모;석태수;신시균;이채식;강태경
    • Journal of Biosystems Engineering
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    • 제31권3호
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    • pp.182-187
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    • 2006
  • Aerial application using an unmanned agricultural helicopter can reduce labor and pollution. The development of an agricultural helicopter became urgent for both precise and timely spraying. In this study, a rotor system for unmanned helicopter capable of 20 $kg_f$ payload, was developed and lift capability was evaluated. A lift force over the dead weight of the helicopter was obtained at the pitch angle of $6^{\circ}$. As the pitch angle increased to $8^{\circ}\;and\;10^{\circ}$, the total lift increased to $74{\sim}81\;kg_f\;and\;86{\sim}93\;kg_f$, respectively. A range of engine speed at the rated flight condition, lifting mean payload of 23 $kg_f$ was determined. The data acquired from this study will be used for designing tail system and RF console in the next stage of the research. The rated lift capability was enough for loading 20 liters of spray material including spraying equipments.

Development of Intelligently Unmanned Combine Using Fuzzy Logic Control -(Graphic Simulation)-

  • N.H.Ki;Cho, S.I.
    • 한국농업기계학회:학술대회논문집
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    • 한국농업기계학회 1993년도 Proceedings of International Conference for Agricultural Machinery and Process Engineering
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    • pp.1264-1272
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    • 1993
  • The software for unmanned control of three row typed rice combine has been developed using fuzzy logic. Three fuzzy variables were used : operating status of combine, steering, and speed. Eleven fuzzy rules were constructed and the eleven linguistic variables were used for the fuzzy rules. Six sensors were use of to get input values and sensor input values were quantified into 11 levels. The fuzzy output was infered with fuzzy inferrence which uses the correlation product encoding , and it must have been defuzzified by the method of center of gravity to use it for the control. The result of performance test using graphic simulation showed that the intelligently unmanned control of a rice combine was possible using fuzzy logic control.

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농용 무인헬리콥터의 원심클러치 설계 - 동력 전달의 이론분석 - (Centrifugal Clutch Design for an Unmanned Helicopter - Theoretical Analysis of Power Transfer -)

  • 이재홍;구영모;신시균
    • Journal of Biosystems Engineering
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    • 제33권1호
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    • pp.14-20
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    • 2008
  • An agricultural unmanned helicopter was suggested for an alternative to current pesticide application methods to solve such problems as high cost, low efficiency, shirking task and unsafe work. To pursuit this trend, researches on the development of unmanned helicopters have been accelerated in Korea as well. In this research, a guide type centrifugal clutch that plays an important role in the unmanned helicopter was studied. Theoretical analyses and experimental tests were conducted for designing an optimal clutches. Main design factors of the guide type centrifugal clutch were found to be spring constant, free length of spring, mass of friction sector, contact area, allowable pressure, number of friction sector, friction coefficient, radius of drum, and clutch arrangement. And these design factors could be the functions of engaging engine speed and desired power transfer capacity. The result of the single clutch test showed the power transfer capacity of 14.1 PS at 5,800 rpm and the result of the dual clutch test showed that the capacity of 17.7 PS at 5,600 rpm. These experimental results agreed well the theoretical simulations.