• Title/Summary/Keyword: aerial control

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A Study on the MAC(Media Access Control) protocol for Unmanned Aerial Vehicle(UAV) (무인항공기의 매체접속제어 프로토콜 적용에 관한 연구)

  • Jo, Yun-Hyun;Yoon, In-Seop;Kim, Sang-Uk;Park, Hyo-Dal
    • The Journal of the Korea institute of electronic communication sciences
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    • v.11 no.1
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    • pp.119-124
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    • 2016
  • In this paper, we studied on MAC(Media Access Control) protocol for UAVs application. According to the number of UAVs, ground control station should control properly increased UAVs. So, we applied CSMA/CA that used in current civil aircraft to UAV communications and verified the applicability through comparison of throughput and delays of data with various message sizes, In the results, we confirmed applicability for UAVs MAC protocol.

Vision Based Estimation of 3-D Position of Target for Target Following Guidance/Control of UAV (무인 항공기의 목표물 추적을 위한 영상 기반 목표물 위치 추정)

  • Kim, Jong-Hun;Lee, Dae-Woo;Cho, Kyeum-Rae;Jo, Seon-Yeong;Kim, Jung-Ho;Han, Dong-In
    • Journal of Institute of Control, Robotics and Systems
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    • v.14 no.12
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    • pp.1205-1211
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    • 2008
  • This paper describes methods to estimate 3-D position of target with respect to reference frame through monocular image from unmanned aerial vehicle (UAV). 3-D position of target is used as information for surveillance, recognition and attack. In this paper. 3-D position of target is estimated to make guidance and control law, which can follow target, user interested. It is necessary that position of target is measured in image to solve 3-D position of target. In this paper, kalman filter is used to track and output position of target in image. Estimation of target's 3-D position is possible using result of image tracking and information of UAV and camera. To estimate this, two algorithms are used. One is methode from arithmetic derivation of dynamics between UAV, carmer, and target. The other is LPV (Linear Parametric Varying). These methods have been run on simulation, and compared in this paper.

Design and Control of a Quad-Rotor (쿼드로터 비행체의 설계 및 제어)

  • Shim, Sanghyun;Kim, Ji-Chul;Yang, Sungwook;Cheon, Dong-Ik;Lee, Sangchul;Oh, Hwa-Suk;Kang, Min-Young;Keum, Dong-Kyo
    • Journal of Aerospace System Engineering
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    • v.3 no.1
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    • pp.36-41
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    • 2009
  • Quad-rotor is one kind of a rotorcraft in Unmanned Aerial Vehicle (UAV), which consists of four rotors in total and fixed-pitch blades located at the four corners. This vehicle is emerging as popular platform for UAV research due to the simplicity of its construction, the ability of hovering and the vertical take-off and landing (VTOL) capability, etc. Because of those specific capabilities, this vehicle can be applied to many fields: search and rescue, mobile sensor networks, fire observation, etc. However a quad-rotor is much affected by the disturbance due to the characteristics of structure. So this vehicle needs attitude control for stabilizing. In this paper, we design the control law for automatic stabilization. The PID controller is used to control a brushless DC motor. And an accelerometer is used to measure the roll and pitch angles of a quad-rotor.

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Interoperability Design and Verification of Small Drone System Applying STANAG 4586 (STANAG 4586을 적용한 소형드론시스템의 상호운용성 설계 및 검증)

  • Jonghun, Lee;Taesan, Park;Kilyoung, Seong;Gyeongrae, Nam;Jungho, Moon
    • Journal of Aerospace System Engineering
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    • v.16 no.6
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    • pp.74-80
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    • 2022
  • The utilisation of small drones is becoming increasingly widespread particularly in the military sector. In this study, STANAG 4586, a standard interface for military unmanned aerial vehicles, was applied to a multicopter-type small drone to examine the suitability of the military system. To accomplish this, a small multi-copter vehicle was designed and manufactured, integrating a flight control computer, ground control system, and data link. Furthermore, flight control and ground control equipment software were developed by applying the STANAG 4586 interface, followed by HILS and flight tests.

Location Accuracy of Unmanned Aerial Photogrammetry Results According to Change of Number of Ground Control Points (지상기준점 개수 변화에 따른 무인항공 사진측량 성과물의 위치 정확도 분석)

  • YUN, Bu-Yeol;SUNG, Sang-Min
    • Journal of the Korean Association of Geographic Information Studies
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    • v.21 no.2
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    • pp.24-33
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    • 2018
  • DSM and orthoimage, which are representative results of UAV photogrammetry, are high-quality spatial information data and are widely used in various fields of spatial information industry in recent years. However, the UAV photogrammetry has a problem that the quality of the output of the UAV deteriorates due to the altitude of the UAV, the camera calibration, the weather conditions at the time of shooting, the performance of the GPS / IMU and the number of the ground reference points. The purpose of this study is to analyze the location accuracy of unmanned aerial photogrammetry according to the change of the number if ground control points. Experiments were made with fixed wing, and the shooting altitude was set at 130m and 260m. The number of ground reference points used was 9, 8, 5, and 4, respectively. Ten checkpoints were used. XY RMSE for orthoimage and Z RMSE for DSM were compared and analyzed. In addition, the resolution of the orthoimage was determined to affect the judgment of the operator in the verification of the planimetric position accuracy, and the visual resolution was analyzed using the Siemens star target. As a result of the analysis, the variation of the vertical position accuracy is larger than the variation of the planimetric position accuracy when the number of the ground reference points are different. Also The higher the flying height, the greater the effect of change of ground control points on position accuracy.

A Study on Data Acquisition in the Invisible Zone of UAV through LTE Remote Control (LTE 원격관제를 통한 UAV의 비가시권 데이터 취득방안)

  • Jeong, HoHyun;Lee, Jaehee;Park, Seongjin
    • Korean Journal of Remote Sensing
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    • v.35 no.6_1
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    • pp.987-997
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    • 2019
  • Recently the demand for drones is rapidly increasing, as developing Unmanned Aerial Vehicle (UAV) and growing interest in them. Compared to traditional satellite and aerial imagery, it can be used for various researches (environment, geographic information, ocean observation, and remote sensing) because it can be managed with low operating costs and effective data acquisition. However, there is a disadvantage in that only a small area is acquired compared to the satellite and an aircraft, which is a traditional remote sensing method, depending on the battery capacity of the UAV, and the distance limit between Ground Control System (GCS) and UAV. If remote control at long range is possible, the possibility of using UAV in the field of remote sensing can be increased. Therefore, there is a need for a communication network system capable of controlling regardless of the distance between the UAV and the GCS. The distance between UAV and GCS can be transmitted and received using simple radio devices (RF 2.4 GHz, 915 MHz, 433 MHz), which is limited to around 2 km. If the UAV can be managed simultaneously by improving the operating environment of the UAV using a Long-Term Evolution (LTE) communication network, it can make greater effects by converging with the existing industries. In this study, we performed the maximum straight-line distance 6.1 km, the test area 2.2 ㎢, and the total flight distance 41.75 km based on GCS through LTE communication. In addition, we analyzed the possibility of disconnected communication through the base station of LTE communication.

The Study of Aerial Triangulation Using GPS (GPS를 이용한 사진기준점 측랑에 관한 연구)

  • 이재원;문두열;김정희;김진수
    • Spatial Information Research
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    • v.12 no.2
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    • pp.181-191
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    • 2004
  • Nowadays, GPS-photogrammetry can be applied to the basemap production, a land register and NGIS. And from now on, as the increase of GPS receiver rate, the study on the interpolation methods considering the exact movement of an aircraft at photoflight and the study on the supplement of GPS defect by INS are required continuously. GPS-Photogrammetry, which are based on the direct measurement of the projection centers and attitude at the moment of camera exposure time through loading the GPS receiver in aircraft. This photogrammetric methods can of for us to acquire the exterior orientation parameters with only minimum ground control points, even the ground control process could be completely skipped. Consequently, we can drastically reduce the time and cost far the mapping process. In this thesis, two test flights were conducted in area to evaluate the performance of accuracy and efficiency through the analysis of results between the two photogrammetric methods, that is, traditional photograrammetry, GPS-Photogrammetry. Test results shows that a large variety of advantages of GPS-Photogrammetry against traditional photogrammetry is to be verified. Especially, the number of ground control points for the exterior orientation could be saved more than 70~80%, and the cost far map production 30~50%, respectively. In addition, it was convinced that the large reduction of control points has not any effect on the block accuracy.

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Development of Indoor Navigation Control System for Swarm Multiple AR.Drone's (실내 환경에서의 AR.Drone 군집 비행 시스템 개발)

  • Moon, SungTae;Cho, Dong-Hyun;Han, Sang-Hyuck;Rew, DongYoung;Gong, HyunCheol
    • Aerospace Engineering and Technology
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    • v.13 no.1
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    • pp.166-173
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    • 2014
  • Recently, small quadcopters have been widely used in various areas ranging from military to entertainment applications because interest in the quadcopter increases. Especially, the research on swarm flight which control quadcopters simultaneously without any collision can increase success probability of a important mission. In addition the swarm flight can be applied for demonstrating choreographed aerial maneuvers such as dancing and playing musical instruments. In this paper, we introduce multiple AR.Drone control system based on motion capture for indoor environment in which quadcopters can recognize current position each other and perform scenario based mission.

Intuitive Controller based on G-Sensor for Flying Drone (비행 드론을 위한 G-센서 기반의 직관적 제어기)

  • Shin, Pan-Seop;Kim, Sun-Kyung;Kim, Jung-Min
    • Journal of Digital Convergence
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    • v.12 no.1
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    • pp.319-324
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    • 2014
  • In recent years, high-performance flying drones attract attention for many peoples. In particular, the drone equipped with multi-rotor is expanding its range of utilization in video imaging, aerial rescue, logistics, monitoring, measurement, military field, etc. However, the control function of its controller is very simple. In this study, using a G-sensor mounted on a mobile device, implements an enhanced controller to control flying drones through the intuitive gesture of user. The implemented controller improves the gesture recognition performance using a neural network algorithm.

Linear Distributed Passive Target Tracking Filter for Cooperative Multiple UAVs (다중 UAV 협업을 위한 선형 분산 피동 표적추적 필터 설계)

  • Lee, Yunha;Kim, Chan-Young;Ra, Won-Sang;Whang, Ick-Ho
    • The Transactions of The Korean Institute of Electrical Engineers
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    • v.67 no.2
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    • pp.314-324
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    • 2018
  • This paper proposes a linear distributed target tracking filter for multiple unmanned aerial vehicles(UAVs) sharing their passive sensor measurements through communication channels. Different from the conventional nonlinear filtering schemes, the distributed passive target tracking problem is newly formulated within the framework of a linear robust state estimation theory incorporated with a linear uncertain measurement equation including the coordinate transform uncertainty. To effectively cope with the performance degradation due to the coordinate transform uncertainty, a linear consistent robust Kalman filter(CRKF) theory is devised and applied for designing a distributed passive target tracking filter. Through the simulations for typical UAV surveillance mission, the superior performance of the proposed method over the existing schemes of distributed passive target tracking are demonstrated.