• Title/Summary/Keyword: Redundant Thrusters

Search Result 4, Processing Time 0.018 seconds

Reconfiguration of Redundant Thrusters by Allocation Method

  • Jin, Jae-Hyun;Tahk, Min-Jea
    • International Journal of Aeronautical and Space Sciences
    • /
    • v.6 no.2
    • /
    • pp.76-83
    • /
    • 2005
  • Thrusters are important actuators where air is rare. Since the maintenance or replacement of thrusters is not easy in such an environment, a thrusting system must be highly reliable. Redundant thrusters are used to meet the reliability requirement. In this paper, a reconfiguration problem for those redundant thrusters is discussed, especially the management or distribution logic of redundant thrusters is focused on. The logic has to be changed if faults occur at thrusters. Reconfiguration is to change the distribution logic to accommodate thrusters' faults. The authors propose a reconfiguration algorithm based on the linear programming method. The authors define the reconfiguration problem as an optimization problem. The performance index is a quantity related with total fuel consumption by thrusters. This algorithm can accommodate multiple faults. Numerical examples are given to show the advantage of the proposed algorithm over existing methods.

Control of a Satellite's Redundant Thrusters by a Control Allocation Method (여유 조종력 할당기법을 이용한 인공위성의 여유 추력기 제어)

  • Jin, Jae-Hyun;Park, Young-Woong;Park, Bong-Kyu;Tahk, Min-Jea
    • Journal of the Korean Society for Aeronautical & Space Sciences
    • /
    • v.32 no.10
    • /
    • pp.60-66
    • /
    • 2004
  • Redundant thrusters are generally adopted to satellite designs for a highly reliable attitude control system. So efficient redundancy management is required to take advantage of these redundant thrusters. In this paper, control allocation method is proposed as a method for controlling redundant thrusters. Control allocation is a method to calculate optimal distribution on redundant controls for realizing desired forces/torques. It is shown that a control allocation problem for redundant thrusters is formulated as a linear programming problem which minimizes fuel consumptions with thrusters, constraints. We also show that the proposed method is more efficient than an existing method by numerical examples.

Implementation of Heading Angle and Depth Keeping Control of ROV with Multiple Thrusters by Thrust Allocation (다수의 추진기를 지닌 ROV의 추력배분을 통한 정지 상태에서의 선수각 및 수심 제어 구현)

  • Yoon, Suk-Min;Lee, Chong-Moo;Kim, Kihun
    • Journal of Ocean Engineering and Technology
    • /
    • v.32 no.1
    • /
    • pp.68-75
    • /
    • 2018
  • This study deals with the heading angle and depth keeping control technique for an ROV with multiple horizontal and vertical thrusters by thrust allocation. The light work class ROV URI-L, which is under development at KRISO, is a redundant actuating system with multiple thrusters that are larger than the ROV's degree of freedom. In the redundant actuating system, there are several solutions for a specific ROV motion to be performed. Therefore, a thrust allocation algorithm that considers the entire propulsion system should be regarded as important. First, this paper describes the propulsion system of the ROV and introduces the thrust allocation method of each motion controller. In addition, the performance of the controller is examined using a heading angle and depth keeping control test in a stationary state.

Design and Control of 6 D.O.F(Degrees of Freedom) Hovering AUV (6자유도 호버링 AUV의 설계 및 제어)

  • Jeong, Sang-Ki;Choi, Hyeung-Sik;Seo, Jung-Min;Tran, Ngoc Huy;Kim, Joon-Young
    • Journal of Institute of Control, Robotics and Systems
    • /
    • v.19 no.9
    • /
    • pp.797-804
    • /
    • 2013
  • In this paper, a study of a new hovering six dof underwater robot with redundant horizontal thrusters, titled HAUV (hovering AUV), is presented. The results of study on the structure design, deployment of thrusters, and development of the developed control system of the AUV was presented. For the HAUV structure, a structure design and an analysis of the thrusting system was performed. For navigation, a sensor fusion board which can proceed various sensor signals to identify correct positions and speeds was developed and a total control system including EKF (Extended Kalman Filter) was designed. Rolling, pitching and depth control tests of the HAUV have been performed, and relatively small angle error and depth tracking error results were shown.