• Title/Summary/Keyword: Throttle Control

Search Result 175, Processing Time 0.02 seconds

VEHICLE LONGITUDINAL AND LATERAL STABILITY ENHANCEMENT USING A TCS AND YAW MOTION CONTROLLER

  • Song, J.H.;Kim, H.S.;Kim, B.S.
    • International Journal of Automotive Technology
    • /
    • v.8 no.1
    • /
    • pp.49-57
    • /
    • 2007
  • This paper proposes a traction control system (TCS) that uses a sliding mode wheel slip controller and a PID throttle valve controller. In addition, a yaw motion controller (YMC) is also developed to improve lateral stability using a PID rear wheel steering angle controller. The dynamics of a vehicle and characteristics of the controllers are validated using a proposed full-car model. A driver model is also designed to steer the vehicle during maneuvers on a split ${\mu}$ road and double lane change maneuver. The simulation results show that the proposed full-car model is sufficient to predict vehicle responses accurately. The developed TCS provides improved acceleration performances on uniform slippery roads and split ${\mu}$ roads. When the vehicle is cornering and accelerating with the brake or engine TCS, understeer occurs. An integrated TCS eliminates these problems. The YMC with the integrated TCS improved the lateral stability and controllability of the vehicle.

Development of the VR Simulation System for the Dynamic Characteristics of the Adaptive Cruise Controlled Vehicle (ACC 차량의 동특성 해석을 위한 VR 시뮬레이션 시스템 개발)

  • Kwon, Seong-Jin;Jang, Suk;Yoon, Kyoung-Han;Suh, Myung-Won
    • Transactions of the Korean Society of Automotive Engineers
    • /
    • v.12 no.4
    • /
    • pp.163-172
    • /
    • 2004
  • Nowadays, to analyze the dynamic characteristics of the automotive driving system, the computer simulation linked up with VR(Virtual Reality) technology is treated as the useful method with the improvement of computing ability. In this paper, the VR simulation system has been developed to investigate the driving characteristics of the ASV(Advanced Safety Vehicle) equipped with an ACC(Adaptive Cruise Control) system. For the purpose, VR environment which generates 3D graphic and sound information of the vehicle, the road, the facilities, and the terrain has been organized for the driving reality. Mathematical models of vehicle dynamic analysis including the ACC model have been constructed for computer simulation. The ACC modulates the throttle and brake functions to regulate the vehicle speed so that vehicles could keep proper spacing. Also, the real-time simulation algorithm synchronizes vehicle dynamic simulation with the graphic rendering. With the developed VR simulation system, simple scenarios are applied to analyze the dynamic characteristics. It is shown that the VR simulation system could be useful to evaluate the adaptive cruise controlled vehicle on various driving conditions.

Put Investigation on the energy saving method using inverter driving for cooling pump at MMU training ship (인버터 구동방식에 의한 실습선 냉각수 펌프의 에너지 절감 방법)

  • Lim, Myeong-Hwan;Ahn, Byong-Won;Kim, Bu-Gi
    • Journal of Advanced Marine Engineering and Technology
    • /
    • v.33 no.6
    • /
    • pp.880-885
    • /
    • 2009
  • The ships have a lot of electric machinery needed to supply electricity from the moment of launching coming out of dry dock to docking at jetty. Thus, the ships always have to use alternator and electric machinery that has low efficiency under the low load. Many government service ships like the MMU training ship have been spending lots of time at jetty rather than sailing at sea. These ships are operated under the condition of low load due to the operation of basic machinery at jetty and electric machineries are driven with the status of low efficiency. This paper would suggest the energy saving method for these ships. The investigation describes that shore connection is a great asset to these ships and that the flow rate control by adjusting revolution with the adoption of inverter is better than flow rate control by using throttle valve to save energy. The result is based on the investigation of cooling pump at MMU training ship.

Pressure Control of Staged Combustion Liquid Rocket Engine (다단연소사이클 액체 로켓엔진의 압력제어에 대한 연구)

  • Hwang, Changhwan;Lee, Kwangjin;Woo, Seongphil;Im, Ji-Hyuk;Jeon, Junsu;Lee, Jungho;Yoo, Byungil;Han, Yeoungmin
    • Proceedings of the Korean Society of Propulsion Engineers Conference
    • /
    • 2017.05a
    • /
    • pp.88-93
    • /
    • 2017
  • For the control of pre-burner combustion pressure, the open angle of TTR(Throttle for Thrust Regulation) valve was varied from $143^{\circ}$ to $185^{\circ}$ while testing of cold flow, ignition, combustion. The major performance variables of rocket engine and hydraulic performance of TTR valve regarding the open angle was verified. However the controllability of pre-burner combustion pressure was not verified due to the limitations of test. The comprehensive research will be done after supplementing these problems.

  • PDF

Calculation of the Transfer Function for a Liquid Rocket Engine using a Dynamic Model (액체로켓 엔진의 동특성 모델을 이용한 전달함수의 계산)

  • Park, Soon-Young;Lee, Eun-Seok
    • Proceedings of the Korean Society of Propulsion Engineers Conference
    • /
    • 2012.05a
    • /
    • pp.436-442
    • /
    • 2012
  • In the process of liquid rocket engine design, obtaining method of the dynamic characteristics of engine should be emphasized typically to determine the control logic and algorithms of the throttle valves in the propellant feed pipeline. However, determining the dynamic characteristics of an engine through the autonomous test is very hard and laborious, so that the numerical approach is prevailing. In this study, using the previously developed dynamic analysis model of the engine around the steady state, we introduced a disturbance to this model, and obtained the dynamic response in the time domain. And by applying the well-known Levy method to this temporal response, we could deduce the transfer function of that system that can give us various information of engine and can be manipulated to design the control system.

  • PDF

Fuel Injection Control of Vehicles Using Fuzzy Control Technique (퍼지 제어 기법을 이용한 차량의 연료 제어)

  • Kim, Kwang-Baek;Woo, Young-Woon;Ha, Sang-An
    • Journal of the Korea Institute of Information and Communication Engineering
    • /
    • v.11 no.5
    • /
    • pp.1013-1018
    • /
    • 2007
  • In general, there are many sensors for fuel injection control such as an air flow sensor, an air intake temperature sensor, a cooling water temperature sensor, a throttle position sensor, and a motor position sensor. In this paper, we proposed a method for controlling the amount of fuel consumption in cars using fuzzy control technique by temperature change of an air intake temperature sensor and air-fuel ratio, the ratio of air and fuel mixture. In the proposed method, the amount of fuel injection is controlled by fuzzy membership functions and fuzzy inference rules established for air-fuel ratio, air intake temperature, and final fuel compensation, after computing air-fuel values using each amount of air intake and each amount of fuel injection. We verified that the proposed method is more efficient than conventional methods in fuel injection control from the results of the simulation program.

Step-by-step Tests for Continuous Thrust Control Hot-firing Test (연속 추력제어 연소시험을 위한 단계별 시험들)

  • Cheolwoong Kang;Shinwoo Lee;Sunwoo Han;Kangyeong Lee ;Hadong Jung;Dongwoo Choi;Kyubok Ahn
    • Journal of the Korean Society of Propulsion Engineers
    • /
    • v.27 no.1
    • /
    • pp.58-67
    • /
    • 2023
  • Results of dry-run tests, cold-flow tests, and hot-firing tests performed to throttle a methane engine uni-element thrust chamber are covered in the paper. After installing flow control valves on the oxidizer and fuel supply lines of the methane engine combustion test facility, a number of dry-run tests were repeated so that the valves could reach set strokes quickly and stably. Then, cold-flow tests using liquid nitrogen and gaseous nitrogen were conducted to confirm the stable supply of the simulated propellants according to the valve control. Finally, using liquid oxygen and gaseous methane, hot-firing tests for fixed and continuous thrust control of 50% to 10% of the nominal thrust were successfully performed.

Suggestion of Logic to Control Power Plant Equipped ESS in case of Full Open Turbine Control Valve (ESS를 이용한 발전소 터빈제어밸브 전개 운전 제어로직 제안)

  • In Young Chung;Jae-Heon Lee
    • Plant Journal
    • /
    • v.18 no.4
    • /
    • pp.66-72
    • /
    • 2023
  • In order to respond to the demand for flexible operation of thermal power generation, development of natural sliding pressure operation that minimizes throttle loss by opening the turbine control valve 100% and maximize power generation efficiency in conjunction with ESS in order to quickly respond to fluctuations in the system frequency is required. The logic development of natural sliding pressure operation with ESS was developed to modify the existing logic at the power plant's top-level control logic such as the unit master, the boiler master and the turbine master. Cooperative control algorithms that complement the advantages and disadvantages of ESS operation (quick response, limited capacity) and power plant operation (slow response, continuous operation) not only improve efficiency when applied to actual power plants, but also respond quickly and flexibly to load demands to ensure system stability.

  • PDF

An Automatic Collision Avoidance System for Drone using a LiDAR sensor (LiDAR 센서를 이용한 드론 자동 충돌방지 시스템)

  • Chong, Ui-Pil;An, Woo-Jin;Kim, Yearn-Min;Lee, Jung-Chul
    • Journal of the Institute of Convergence Signal Processing
    • /
    • v.19 no.2
    • /
    • pp.54-60
    • /
    • 2018
  • In this paper, we propose an efficient automatic control method for the collision avoidance of drones. In general, the drones are controlled by transmitting to the flight control (FC) module the received PWM signals transmitted from a RC controller which transduce movements of the knob into PWM signal. We implemented the collision avoidance module in-between receiver and FC module to monitor and change the throttle, pitch and roll control signals to avoid drone collision. In order to avoid the collision, a LiDAR distance sensor and a servo-motor are installed and periodically measure the obstacle distance within -45 degrees from 45 degrees in flight direction. If the collision is predicted, the received PWM signal is changed and transmitted to the FC module to prevent the collision. We applied our proposed method to a hexacopter and the experimental results show that the safety is improved because it can prevent the collision caused by the inadvertency or inexperienced maneuver.

Development of an intuitive motion-based drone controller (직관적 제어가 가능한 드론과 컨트롤러 개발)

  • Seok, Jung-Hwan;Han, Jung-Hee;Baek, Jun-Hyuk;Chang, Won-Joo;Kim, Huhn
    • Design & Manufacturing
    • /
    • v.11 no.3
    • /
    • pp.41-45
    • /
    • 2017
  • Drones can be manipulated in a variety of ways. One of the most common controller is joystick method. But joystick controller uses both hands and takes a long time to learn. Particularly, in the case of 8-character flight, it is necessary to use both front and rear flight (pitch), left and right flight (Roll), and body rotation (Yaw). Joystick controller has limitations to intuitively control it. In particular, when the main body rotates, the viewpoint of the forward direction is changed between the drones and the user, thereby causing a mental rotation problem in which the user must control the rotating state of the drones. Therefore, we developed a motion matching controller that matches the motion of the drones and the controller. That is, the movement of the drone and the movement of the controller are the same. In this study, we used a gyro sensor and an acceleration sensor to map the controller's forward / backward, left / right and body rotation movements to drone's forward / backward, left / right, and rotational flight motion. The motor output is controlled by the throttle dial at the center of the controller. As the motions coincide with each other, it is expected that the first drone operator will be able to control more intuitively than the joystick manipulator with less learning.