• Title/Summary/Keyword: Vehicle Trajectory Analysis

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Behavior and Durability Analysis of Tractor applying a hybrid power system (하이브리드 동력시스템을 적용한 트랙터의 동적 거동 및 내구해석)

  • Kim, Byeong Sam;Lim, Gwang Gue
    • Journal of Auto-vehicle Safety Association
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    • v.6 no.2
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    • pp.61-66
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    • 2014
  • This paper described on the motion of hybrid tractor trajectory for powertrain system. The dynamics behavior used to the tractor according to the characteristics of the road surface using $Daful^@$ analysis. The tractor industry is facing to a big problem about rising gas price and exhaust gas environment. Because it was possible overcoming the past drawback, hybrid vehicle had been decided as the best technical way since it has started operating the internal combustion engine with the electric power as the motive power. The vehicle structures have designed the model of a major power transmission factor. The simulation realized in this paper that motion of tractor being turned by torque and force of each joints. Driving characteristics, especially in recent years, IVHS (Intelligent Vehicle Tractor / System) technology, while receiving a lot of attention because of the tractor and the need to pursue high function is emerging as a more and more.

Trajectory and Attitude Analysis for the 1st Flight Test of KSLV-I Launch Vehicle (나로호 발사체 1차 비행시험에서의 궤적 및 자세 분석)

  • Roh, Woong-Rae;Cho, Sang-Bum;Ko, Jeong-Hwan;Sun, Byung-Chan;Kim, Jeong-Yong;Park, Jeong-Joo;Cho, Gwang-Rae
    • Journal of the Korean Society for Aeronautical & Space Sciences
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    • v.38 no.3
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    • pp.213-220
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    • 2010
  • This paper presents the analysis results of trajectory, performance and attitude control based on the first flight data of the KSLV-I. The KSLV-I had a fairing separation problem and failed to inject spacecraft into the orbit. In this paper, the trajectory, flight performance, and attitude control was analyzed considering the influence of unseparated fairing. Moreover, the flight results and performance of the inertial navigation and guidance system were presented. As a results of post-flight analysis, any other problem besides the fairing separation problem was not happened and onboard equipment functioned normally.

Design of Chicane Based on Vehicle Movement Trajectory (자동차 이동 궤적을 고려한 시케인 설계)

  • Kim, Yong Seok;Lee, Suk Ki
    • International Journal of Highway Engineering
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    • v.14 no.6
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    • pp.159-165
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    • 2012
  • PURPOSES : The lack of details of guidelines on how to install the Chicane for traffic calming leads the practical difference across the calming areas, so the benefits expected from these facilities are not hardly observed. In this context, this study analysed the relationship between the geometric design alternatives of Chicane with the dynamic behaviour of vehicles in terms of speed and trajectory. METHODS : The study analysed vehicle dynamic behaviour using dynamic analysis program Auto-Turn under various geometric conditions of Chicane. RESULTS : This study suggested the design alternatives of Chicane using terms such as "longitudinal displacement value", "lateral displacement value", etc. which are defined in the study. The suggested combination set is fulfilling the desired or target speed of vehicles and clearance between vehicle and roadside at the same time. CONCLUSIONS : The results from this study can be applied to install Chicane corresponding to the local condition where target speed is 30km/h. The study showed the design alternatives of chicane corresponding to the given road cross-sectional design and clearance to roadside for passenger cars and light truck respectively.

Performance Analysis of a UAV Energy Harvesting Relay Network in the Terahertz Band (테라헤르츠 대역 무인비행체 에너지 수확 릴레이 네트워크 성능분석)

  • Yeongi Cho;Saifur Rahman Sabuj;Han-Shin Jo
    • Journal of IKEEE
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    • v.27 no.4
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    • pp.411-417
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    • 2023
  • Unmanned aerial vehicle (UAV)-assisted relay has the advantages of ease of deployment, good communication channels, and mobility over traditional terrestrial relay, which greatly improves wireless connectivity. In this paper, we design a UAV-enabled relay network that can utilize radio frequency bands to harvest energy from sources and utilize terahertz (THz) bands to transmit information between secondary transmitters and receivers. Next, we solve the optimal position of the UAV that maximizes the relay channel capacity, and propose an algorithm to design two trajectories of UAV (a straight and an elliptical trajectory) using the derived solution. Numerical results show that the straight trajectory is better in terms of harvested energy and channel capacity.

Analysis of Intelligent Vehicle Control Methods for CIM at Non-signalized Intersections (비 신호 교차로에서 CIM을 위한 지능형 차량 제어기법 분석)

  • Joo, Hyunjin;Lim, Yujin
    • Asia-pacific Journal of Multimedia Services Convergent with Art, Humanities, and Sociology
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    • v.8 no.2
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    • pp.33-40
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    • 2018
  • There are lots of literature about connected car system from industry and academia. The connected car is a smart car integrated with IT technology that is connected to people, vehicles and traffic management systems. It is important to V2I (vehicle to infrastructure) communication which is the connection between the vehicle and the infrastructure. CIM (cooperative intersection management) is a device to manage the communication between vehicle and infrastructure. In this paper, we analyze two intelligent vehicle control methods using CIM at non-signalized intersections. In the first method, a vehicle to pass through intersection needs to reserve a resource of intersection. In the second method, trajectory patterns on pre-planned vehicles are classified to pass through intersection. We analyze case studies of two methods to be implemented by DP(dynamic programming) and ACO(ant colony optimization) algorithms. The methods can be reasonably improved by placing importance on vehicles or controlling speeds of vehicles.

Intelligent Vehicle Management Using Location-Based Control with Dispatching and Geographic Information

  • Kim Dong-Ho;Kim Jin-Suk
    • Proceedings of the KSRS Conference
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    • 2004.10a
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    • pp.249-252
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    • 2004
  • The automatic determination of vehicle operation status as well as continuous tracking of vehicle location with intelligent management is one of major elements to achieve the goals. Especially, vehicle operation status can only be analyzed in terms of expert experiences with real-time location data with scheduling information. However the scheduling information of individual vehicle is very difficult to be interpreted immediately because there are hundreds of thousand vehicles are run at the same time in the national wide range workplace. In this paper, we propose the location-based knowledge management system(LKMs) using the active trajectory analysis method with routing and scheduling information to cope with the problems. This system uses an inference technology with dispatching and geographic information to generate the logistics knowledge that can be furnished to the manager in the central vehicle monitoring and controlling center.

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Error analysis of underwater vehicle under influence of disturbance and time delay (외란과 시간 지연에 의한 수중 운동체의 오차 해석)

  • 나윤철;이정규;권순홍;이만형
    • 제어로봇시스템학회:학술대회논문집
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    • 1992.10a
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    • pp.845-849
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    • 1992
  • The disturbance and time delay can often cause a significant error in the estimation of trajectory of a underwater vehicle. The time delay considered in this study is due to the delayed rudder response to the rudder input from the guidance control part. The simulation tests are performed on maneuver with constant rudder angle, zigzag maneuver, dive-climb maneuver, and corridor pattern maneuver. The results are compared with those of without delay cases.

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Constant speed, variable ascension rate, helical trajectories for airplanes

  • Labonte, Gilles
    • Advances in aircraft and spacecraft science
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    • v.5 no.1
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    • pp.73-105
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    • 2018
  • A particular type of constant speed helical trajectory, with variable ascension rate, is proposed. Such trajectories are candidates of choice as motion primitives in automatic airplane trajectory planning; they can also be used by airplanes taking off or landing in limited space. The equations of motion for airplanes flying on such trajectories are exactly solvable. Their solution is presented, together with an analysis of the restrictions imposed on the geometrical parameters of the helical paths by the dynamical abilities of an airplane. The physical quantities taken into account are the airplane load factor, its lift coefficient, and the thrust its engines can produce. Formulas are provided for determining all the parameters of trajectories that would be flyable by a particular airplane, the final altitude reached, and the duration of the trajectory. It is shown how to construct speed interval tables, which would appreciably reduce the calculations to be done on board the airplane. Trajectories are characterized by their angle of inclination, their radius, and the rate of change of their inclination. Sample calculations are shown for the Cessna 182, a Silver Fox like unmanned aerial vehicle, and the F-16 Fighting Falcon.

Launch Trajectory Analysis of a Spacecrafta (위성발사체의 발사궤적 해석)

  • 최재원;이장규;이달호
    • 제어로봇시스템학회:학술대회논문집
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    • 1988.10a
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    • pp.614-619
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    • 1988
  • In this paper, an arbitrary mission of a spacecraft from launch to orbit injection is investigated for some launch trajectories. Launch sites are selected arbitrarily from various locations in Korea. For this study, a general purpose simulation program is developed. In this program, the Earth is assumed to be a rotating ellipsold. The launch vehicle is treated as a 3-D, 6-DOF rigid body. The developed program has been evaluated by calibrating it to the 3-stage N-1 rocket developed in Japan and launched at Tanegasima. The simulated trajectory from the first-stage ignition to burnout of third-stage main engine is compared with the previously tested N-1 rocket trajectory in Japan. The result shows that the program works properly. Using the proven program, we have investigated possible launch locations in Korea, namely Marado, Sungsan and Kuryongpo. The problem of polar orbit injection is also examined.

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A Study on Driving Trajectory of AGV for Container Transport (컨테이너 운송용 AGV의 운동궤적에 관한 연구)

  • Lee, Ji-Yong;Kim, Min-Ju;Lee, Seung-Soo;Kim, Joong-Wan;Jeon, Eon-Chan
    • Proceedings of the KSME Conference
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    • 2004.04a
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    • pp.1076-1081
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    • 2004
  • In this study, we have developed the simulation tool in order to investigate driving trajectory of AGV for container transport. AGV for container transport is different from the indoor AGV in that it is a large size structure at being loaded the weight of 40 ton. And AGV for container transport is applied to front wheel steering, rear wheel steering, all wheel steering, and crap steering. Therefore, we have developed the simulation tool considering dynamic problems and center of turning in accordance with four way of steering modes. Throughout some computer simulations, we have confirmed that this tool is useful to analysis dynamic problems and to calculate minimum radius of turning for large size vehicles.

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