• Title/Summary/Keyword: Thrust allocation

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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
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    • v.32 no.1
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    • pp.68-75
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    • 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.

Optimal Thrust Allocation for Dynamic Positioning of Deep-sea Working Vessel

  • Zhao, Luman;Roh, Myung-Il;Hong, Jeong-Woo
    • Journal of Advanced Research in Ocean Engineering
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    • v.1 no.2
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    • pp.94-105
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    • 2015
  • In this study, a thruster allocation method of a deep-sea working vessel was proposed with the aims of producing the demanded generalized forces and moment for dynamic positioning while at the same time minimizing total power. For this, an optimization problem for thrust allocation was mathematically formulated with design variables, objective function, and constraints. The genetic algorithms (GA) was used to solve the formulated problem. The proposed method was applied to an example of finding optimal thrust allocation of the deep-sea working vessel having 5 thrusters. The result showed that the method could be used to determine better strategy for thruster allocation of the vessel as compared to existing study.

Mixed Control of Agile Missile with Aerodynamic Fin and Thrust Vectoring Control (유도탄의 유도명령 추종을 위한 혼합제어기 설계 : 공력 및 추력벡터제어)

  • 이호철;최용석;송택렬;송찬호;최재원
    • Journal of Institute of Control, Robotics and Systems
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    • v.10 no.7
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    • pp.658-668
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    • 2004
  • This paper is concerned with a control allocation strategy using the dynamic inversion and the pseudo inverse control which generates the nominal control input trajectories. In addition, an autopilot design method is proposed by using time-varying control technique which is time-varying version of the pole placement of linear time-invariant system for an agile missile with aerodynamic fin and thrust vectoring control. The control allocation proposed in this paper is capable of extracting the maximum performance by combining each control effector, aerodynamic fin and thrust vectoring control. The adopted time-varying control technique for the autopilot design enhances the robustness of the tracking performance for a reference command. The main results are validated through the nonlinear simulations with aerodynamic data.

Dynamic Positioning Control of a Twin-hull Unmanned Surface Ship (쌍동형 무인선의 동적위치제어에 관한 연구)

  • Kang, Minju;Kim, Taeyun;Kim, Jinwhan
    • The Journal of Korea Robotics Society
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    • v.11 no.4
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    • pp.217-225
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    • 2016
  • Dynamic Positioning (DP) is used to automatically maintain the position and heading of a floating structure subjected to environmental disturbances. A DP control system is composed of a motion controller to compute the desired force and moment and a thrust allocator to distribute the computed force and moment to multiple thrusters considering mechanical and operational constraints. Among various thruster configurations, azimuth thrusters or propeller/rudder pairs tend to make the allocation problem difficult to solve, because these types of propulsion systems include nonlinear constraints. In this paper, a dynamic positioning strategy for a twin-thruster ship that is propelled by two azimuthing thrusters is addressed, and a thrust allocation method which does not require a numerical optimization solver is proposed. The applicability of the proposed method is demonstrated with an experiment using an autonomous boat.

Mixed Control of Agile Missile with Aerodynamic Fin and Thrust Vectoring Control (공력 및 추력을 이용한 유도탄의 혼합제어기 설계(I))

  • 이호철;최용석;최재원;송택렬;송찬호
    • Journal of the Korea Institute of Military Science and Technology
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    • v.6 no.3
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    • pp.122-130
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    • 2003
  • This paper is concerned with a control allocation strategy using the dynamic inversion and the pseudo inverse control which generates the nominal control input trajectories, and autopilot design using time-varying control technique which is time-varying version of pole placement of linear time-invariant system for an agile missile with aerodynamic fin and thrust vectoring control. Control allocation of this paper is capable of extracting the maximum performance from each control effector, aerodynamic fin and thrust vectoring control, by combining the action of them. Time-varying control technique for autopilot design enhance the robustness of the tracking performance for a reference command. The main results are validated through the nonlinear simulation.

Modeling and Development of an Integrated Controller for a Ship with Propellers and Additional Propulsion Units (프로펠러와 부가추력장치를 갖는 특수선의 모델링 및 통합제어기 개발)

  • Kim Jong Hwa;Lim Jae Kwon;Lee Byung Kyul
    • Journal of Advanced Marine Engineering and Technology
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    • v.29 no.2
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    • pp.236-242
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    • 2005
  • Dynamic Positioning(DP) system maintains ship's position (fixed location or predetermined track) exclusively by means of CPPs and thrusters. To generate the control input adequate to various situation an integrated controller for CPPs and thrusters is required. The integrated controller is composed of a thrust calculation algorithm and a thrust allocation algorithm. The thrust calculation algorithm generates thrusts in the surge direction and the sway direction from the desired forward and lateral speed and generates a moment about the yaw axis from desired heading angle. The thrust allocation algorithm allocates the generated thrusts and moment to each CPP and thruster. Computer simulations are executed to confirm the effectiveness of the suggested controller.

Autopilot Design for Agile Missile with Aerodynamic Fin and Thrust Vecotring Control

  • Lee, Ho-Chul;Choi, Yong-Seok;Choi, Jae-Weon
    • 제어로봇시스템학회:학술대회논문집
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    • 2003.10a
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    • pp.525-530
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    • 2003
  • This paper is concerned with a control allocation strategy using the dynamic inversion which generates the nominal control input trajectories, and autopilot design using the time-varying control technique which is time-varying version of pole placement of linear time-invariant system for an agile missile with aerodynamic fin and thrust vectoring control. Dynamic inversion can decide the amount of the deflection of each control effector, aerodynamic fin and thrust vectoring control, to extract the maximum performance by combining the action of them. Time-varying control technique for autopilot design enhance the robustness of the tracking performance for a reference command. Nonlinear simulations demonstrates the dynamic inversion provides the effective nominal control input trajectories to achieve the angle of attack command, and time-varying control technique exhibits good robustness for a wide range of angle of attack.

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Research for Thrust Distribution Method of DACS for Response to Pintle Actuating Failure (DACS 추진기관의 핀틀 구동장치 고장을 허용하는 추력 분배기법 연구)

  • Ki, Taeseok
    • Journal of the Korean Society of Propulsion Engineers
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    • v.21 no.5
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    • pp.61-70
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    • 2017
  • Robust thrust distribution method of solid DACS is researched. For the case of the system which has higher number of actuation nozzles than the degree of freedom of thrust to be controlled, the robust thrust allocation law which accommodate the abnormal operation is suggested. Assuming the situation that some nozzles are uncontrollable, the error between nozzle throat area command and response can be calculated. The error is used for realtime reshaping of weighting matrix. From the weighting effect, the nozzle which operated abnormally has low responsibility for the command then, the thrust error is reduced. The suggested algorithm is verified by the simulation of abnormal operation condition of DCS and ACS nozzle respectively.

A Study on the Development of Dynamic Positioning System for Barge Type Surface Vessels (Barge 형 수상선의 DP(Dynamic Positioning) System 개발에 관한 연구)

  • Bui, Van-Phuoc;Kim, Young-Bok
    • Journal of Power System Engineering
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    • v.16 no.2
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    • pp.66-74
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    • 2012
  • In this paper, the authors propose a new approach to control a barge type surface vessel. It is based on the Dynamic Positioning System(DPS) design. The main role of barge ship is to carry and supply the materials to the floating units and other places. To carry out this job, it should be positioned in the specified area. However sometimes the thrust systems are installed on it, and in general the rope control by mooring winch system is used. It may be difficult to compare the control performances of two types. If we consider this problem in point of usefulness, we can easily find out that the winch control system is more useful and applicable to the real field than the thrust control system except a special use. Therefore, in this paper we consider a DPS design problem which can be extended to the many application fields. The goal of this paper is twofold. First, the sliding mode controller (SMC) for positioning the our vessel is proposed. Especially, in this paper, a robust stability condition is given based on descriptor system representation. In the result, the sliding mode control law guarantees to keep the vessel in the defined area in the presence of environmental disturbances. And second, the thrust allocation problem is solved by using redistributed pseudo-inverse (RPI) algorithm to determine the thrust force and direction of each individual actuator. The proposed approach has been simulated with a supply vessel model and found work well.

Pressure Guidance and Thrust Allocation Law of Solid DACS (고체 추진 DACS의 압력 유도 및 추력 분배기법)

  • Park, Iksoo;Hong, Seokhyun;Ki, Taeseok;Park, Jungwoo
    • Journal of the Korean Society of Propulsion Engineers
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    • v.19 no.2
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    • pp.9-16
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    • 2015
  • The control law for simultaneous pressure and thrust control of solid DACS(Divert Attitude Control System) is suggested. To regulate the two variables effectively, the control structure of sequential loop closer is applied to the system considering the physical characteristics of each variable and the weighted pseudo-inverse method is suggested to allocate effective command for indeterminate system. Also, the pressure guidance law for safe and high acceleration is applied to the homing stage to verify the effectiveness of the command distribution.