http://chineseinput.net/에서 pinyin(병음)방식으로 중국어를 변환할 수 있습니다.
변환된 중국어를 복사하여 사용하시면 됩니다.
Autolanding Mission Planning of the IT Convergence Hoverable UAV
Sunghun Jung,Hyunsu Kim 한국융합학회 2017 한국융합학회논문지 Vol.8 No.6
Li-Po 에너지 밀도의 기술적 진보의 한계로 회전익 무인항공기의 비행시간은 제한적이기 때문에, 연구원들은 회전익 무인항공기의 완전한 자율 임무 수행을 위하여 우회 해결책을 찾고 있다. 몇 가지 후보 해결책들 중, 자동 무선 충전이 가장 가능성 있고 현실적인 후보이며, 본 논문에서는 자동 무선 충전의 주요 기술인 자동 착륙 전략에 초점을 맞추고 있다. MATLAB/Simulink를 기반으로 Li-Po 배터리팩 시뮬레이터를 포함한 회전익 무인항공기 비행 시뮬레이터를 개발하였으며, 이를 통해 비행 상태 및 배터리팩 상태를 분석하였다. 이륙할 때 1,647 W의 최대 모터 출력이 발생하였고, 이때 셀 전압은 최소 3.39 V까지 감소하였다. 이는 22 Ah를 지니고 12S1P로 연결된 2개의 배터리팩이 자동 착륙 임무수행에 적합하다는 것을 나타낸다. Researchers are now faced with a limited flight time of the hoverable UAV due to the sluggish technological advances of the Li-Po energy density and try to find a bypassing solution for the fully autonomous hoverable UAV mission planning. Although there are several candidate solutions, automated wireless charging is the most likely and realistic candidate and we are focusing on the autolanding strategy of the hoverable UAV in this paper since it is the main technology of it. We developed a hoverable UAV flight simulator including Li-Po battery pack simulator using MATLAB/Simulink and UAV flight and battery states are analyzed. The maximum motor power measured as 1,647 W occurs during the takeoff and cell voltage decreases down to 3.39 V during the procedure. It proves that the two Li-Po battery packs having 22 Ah and connected in series forming 12S1P are appropriate for the autolanding mission planning.
System Identification of Quadrotor IT Convergence UAV using Batch and RLS Estimation Methods
Sunghun Jung 한국융합학회 2017 한국융합학회논문지 Vol.8 No.4
무인항공기는 2000년대 중반부터 탐색, 조사, 매핑, 수색 및 구조 등의 3D 작업에 적극적으로 사용되기 시작했다. 이러한 세계적인 추세에 따라, 무인항공기의 정밀한 제어는 엄청난 응용 산업들의 측면에 있어서 혁명을 가져올 것이다. 논문의 첫 번째 파트에서는 시스템식별 기법을 사용하여 간략화 된 무인항공기의 모델을 이전의 이산시간 선형모델과 비교분석 한다. 두 번째 파트에서는 동적 모델의 세 가지 변수가 배치추정기법과 RLS추정기 법을 사용하여 추정된다. 쿼드로터 무인항공기 호버링 기동 시의 각가속도 데이터가 항상 수렴한다고 분석되었다. 또한 실험 및 MATLAB 시뮬레이션의 쿼드로터 무인항공기 비행 데이터에 의하면, 배치추정기법이 RLS추정기법 보다 더 정확하다고 판명되었다. UAVs began to be actively applied to so-called 3D jobs, including the autonomous exploration, investigation, mapping, search and rescue, etc. since the mid-2000s. With this global trend, having a precise controllability of the UAV will certainly revolutionize the life of the modern human in the aspect of tremendous applications of the UAV. In the first part, a simplified dynamic model of the UAV identified using system identification techniques is compared with the previously built time-discrete linear model. In the second part, the three parameters of the dynamic model are estimated using the batch and RLS methods. Angular acceleration data of the quadrotor UAV at the hovering maneuver are analyzed and shown to be converging at all time. Also, according to the quadrotor flight data from both experiments and MATLAB simulations, the batch estimation method turns out to be more accurate than the RLS estimation method based on the comparison of final parameter values.
Automated Wireless Recharging for Small UAVs
Jung, Sunghun,Ariyur, Kartik B. The Korean Society for Aeronautical and Space Scie 2017 International Journal of Aeronautical and Space Sc Vol.18 No.3
We develop a wireless, contact free power transfer mechanism that is safer than the direct metallic contact and robust to imperfect alignment on landing at the base station. A magnetic field is created using inductors on both the transmitting and receiving sides. We use the inductive wireless recharging to increase autonomy and decrease the sensor interference by reducing the inductor loop size. By locating four independent small receiver loops and corresponding four circuits around the quadrotor UAV, we can increase safety from circuit malfunctions in comparison to the use of just one loop. On the base station, four folding robotic bars are used to realign the receiver loops over the transmitter loops. After adequate recharging as measured by battery voltages or power consumption at the bae station, the UAV sends a signal to the base station to open the robotic bars and takes off once freed from the robotic bars.
Robustness for Scalable Autonomous UAV Operations
Jung, Sunghun,Ariyur, Kartik B. The Korean Society for Aeronautical and Space Scie 2017 International Journal of Aeronautical and Space Sc Vol.18 No.4
Automated mission planning for unmanned aerial vehicles (UAVs) is difficult because of the propagation of several sources of error into the solution, as for any large scale autonomous system. To ensure reliable system performance, we quantify all sources of error and their propagation through a mission planner for operation of UAVs in an obstacle rich environment we developed in prior work. In this sequel to that work, we show that the mission planner developed before can be made robust to errors arising from the mapping, sensing, actuation, and environmental disturbances through creating systematic buffers around obstacles using the calculations of uncertainty propagation. This robustness makes the mission planner truly autonomous and scalable to many UAVs without human intervention. We illustrate with simulation results for trajectory generation of multiple UAVs in a surveillance problem in an urban environment while optimizing for either maximal flight time or minimal fuel consumption. Our solution methods are suitable for any well-mapped region, and the final collision free paths are obtained through offline sub-optimal solution of an mTSP (multiple traveling salesman problem).
Strategic Cattle Roundup using Multiple Quadrotor UAVs
Jung, Sunghun,Ariyur, Kartik B. The Korean Society for Aeronautical and Space Scie 2017 International Journal of Aeronautical and Space Sc Vol.18 No.2
Four quadrotor UAVs are maneuvered to guide four animals into their pen within the minimum time by creating noises of predators modeled with an exponential function. The quadrotor UAVs are controlled via PID controllers, follow time optimal trajectories, and avoid collisions through altitude separations. The stability of the proposed PID controller is analyzed and verified using MATLAB/Simulink based simulations. Proposed step by step strategies would be practical solutions of actual cattle roundup problems.