Single-Primary-Winding Current-Fed Multiple-Input Full-Bridge Converter

2012 ◽  
Vol 461 ◽  
pp. 250-254
Author(s):  
Qin Wang ◽  
Mu Yu Cheng ◽  
Lan Xiao ◽  
Lei Wang
Keyword(s):  
Fuel Cell ◽  
Control Strategy ◽  
Control Method ◽  
Current Source ◽  
Flexible Control ◽  
Multiple Input ◽  
Pv Cell ◽  
Multiple Primary ◽  
Simulation Results ◽  
Pulsating Current

This paper proposes the topological generated method, control method and circuit feature of the single primary winding current-fed full-bridge MIC. The MIC has only one primary winding. Compared with the traditional multiple primary winding current-fed MIC, it has simpler structure, more flexible control and can power the load simultaneously or individually. The Pulsating Current Source Cell in the converter is Boost type. The input current is continuous and it can prolong the usage age of PV cell and fuel cell. The single primary winding current-fed double-input full-bridge converter based on Boost converter is taken as an example to analyze its operation principle, control strategy. Simulation results are presented to verify the theoretical analysis

Proposed Topology for Voltage Sag Mitigation with New Control Strategy

2019 ◽  
Vol 15 (2) ◽  
pp. 138-144
Author(s):  
Adnan Diwan ◽  
Khalid Abdulhasan
Keyword(s):  
Duty Cycle ◽  
Control Strategy ◽  
Output Voltage ◽  
System Analysis ◽  
Control Method ◽  
Boost Converter ◽  
Voltage Sag ◽  
Voltage Sags ◽  
Long Duration ◽  
Simulation Results

voltage sags represent the greatest threat to the sensitive loads of industrial consumers, the microprocessor based-loads, and any electrical sensitive components. In this paper, a special topology is proposed to mitigate deep and long duration sags by using a modified AC to AC boost converter with a new control method. A boost converter is redesigned with a single switch to produces an output voltage that is linearly proportional to the duty cycle of the switch. On the other hand, the proposed control system is based on introducing a mathematical model that relates the missing voltage to the duty cycle of the boost converter switch. The simulation results along with the system analysis are presented to confirm the effectiveness and feasibility of the proposed circuit.

scholarly journals Steering Control Method for an Underactuated Unicycle Robot Based on Dynamic Model

2018 ◽  
Vol 2018 ◽  
pp. 1-13
Author(s):  
Hongzhe Jin ◽  
Yang Zhang ◽  
Hui Zhang ◽  
Zhangxing Liu ◽  
Yubin Liu ◽  
...  
Keyword(s):  
Angular Velocity ◽  
Control Strategy ◽  
Pitch Angle ◽  
Control Method ◽  
Steering Control ◽  
Dynamics Model ◽  
Gyroscope System ◽  
Simulation Results ◽  
Balance Structure ◽  
Gyroscope Precession

This paper proposes a lateral balancing structure based on precession effect of double-gyroscopes and its associated control strategy of the steering for an underactuated unicycle robot. Double-gyroscopes are symmetrically designed on the top of the unicycle robot and utilized to adjust the lateral balance of system. Such design can inhibit the disturbance of the gyroscope system to the pitch angle and is beneficial to maintain the lateral balance in the case of large roll angle fluctuations. Based on the analysis of the dynamics model, the gyroscope precession effects will be caused by the angular velocity of the bottom wheel and the roll angular velocity, i.e., resulting in a torque in the direction of the yaw. Then, a rapid response control strategy is proposed to use the torque to control the steering. Simulation results demonstrate the rationality of the lateral balance structure and the feasibility of the steering control method.

scholarly journals Lateral control strategy for a hypersonic cruise missile

2017 ◽  
Vol 14 (2) ◽  
pp. 172988141769914 ◽  
Author(s):  
Yonghua Fan ◽  
Pengpeng Yan ◽  
Hongyang Xu ◽  
Fan Wang
Keyword(s):  
Control Strategy ◽  
Control Method ◽  
Controller Design ◽  
Roll Angle ◽  
Cruise Missile ◽  
Lateral Motion ◽  
Lateral Control ◽  
Optimal Control Method ◽  
Multiple Input ◽  
Combined Control

Hypersonic cruise missile always adopts the configuration of waverider body with the restraint of scramjet. As a result, the lateral motion exhibits serious coupling, and the controller design of the lateral lateral system cannot be conducted separately for yaw channel and roll channel. A multiple input and multiple output optimal control method with integrators is presented to design the lateral combined control system for hypersonic cruise missile. A hypersonic cruise missile lateral model is linearized as a multiple input and multiple output plant, which is coupled by kinematics and fin deflection between yaw and roll. In lateral combined controller, the integrators are augmented, respectively, into the loop of roll angle and lateral overload to ensure that the commands are tracked with zero steady-state error. Through simulation, the proposed controller demonstrates good performance in tracking the command of roll angle and lateral overload.

scholarly journals Dynamical Adaptive Integral Sliding Backstepping Control of Nonlinear Nontriangular Uncertain Systems

2014 ◽  
Vol 2014 ◽  
pp. 1-14 ◽  
Author(s):  
Mahmood Pervaiz ◽  
Qudrat Khan ◽  
Aamer Iqbal Bhatti ◽  
Shahzad Ahmed Malik
Keyword(s):  
Control Strategy ◽  
Uncertain Systems ◽  
Control Method ◽  
Sliding Mode ◽  
Control Law ◽  
Continuous Stirred Tank Reactor ◽  
Adaptive Backstepping ◽  
Recursive Procedure ◽  
Continuous Stirred Tank ◽  
Simulation Results

We present a control strategy for nonlinear nontriangular uncertain systems. The proposed control method is a synergy between the dynamic adaptive backstepping (DAB) and integral sliding mode (ISM) and is referred to as DAB-ISMC. Our main objective is to find a recursive procedure to transform a nontriangular system into an implementable form that enables designing a control law which almost eliminates the reaching-phase. The proposed method further facilitates minimization of chattering which is believed to be a shortcoming of the sliding mode control. In this methodology, the ISM, as an integrated subsystem of DAB, is introduced at the final stage of backstepping. This strategy works very well to obtain a system that is robust against model imperfections, matching and unmatching uncertainties. The DAB-ISMC method is applied on a continuous stirred tank reactor (CSTR) and simulation results obtained on Matlab are found to be very promising.

scholarly journals Flexible control strategy for fuel cell–supercapacitor power system

2017 ◽  
Vol 2017 (13) ◽  
pp. 2580-2583
Author(s):  
Chen Qian ◽  
Qiu Peng ◽  
Wu Jia Yi ◽  
Lu Yi ◽  
Tong Kai ◽  
...  
Keyword(s):  
Fuel Cell ◽  
Power System ◽  
Control Strategy ◽  
Flexible Control

scholarly journals Stabilization of A Single Chamber Single Population Microbial Fuel Cell by Using of a Novel Nonlinear Adaptive Sliding Mode Control

2021 ◽  
Vol 24 (1) ◽  
pp. 14-20
Author(s):  
Xiuwei Fu ◽  
Li Fu ◽  
Hashem Imani Marrani
Keyword(s):  
Fuel Cell ◽  
Microbial Fuel Cell ◽  
Control Method ◽  
Sliding Mode ◽  
Adaptive Sliding Mode Control ◽  
Single Population ◽  
Simulation Results ◽  
The Stability ◽  
Classical Control ◽  
Combined Technique

The microbial fuel cell is one of the most important tools in the supply of renewable energy and its controller plays an important role in improving the performance and stability of its output. Using the advantages of adaptive and sliding mode methods, this paper presents a combined technique to ensure the stability and output voltage stabilization of the fuel cell in the presence of parametric uncertainties and nonlinear terms. The proposed control method is compared with classical control approaches and the simulation results confirm its efficiency.

Control Strategy of the Dual Motors Coupling Propulsion for Battery Electric Buses

2014 ◽  
Vol 528 ◽  
pp. 364-370 ◽  
Author(s):  
Guang Wei Han ◽  
Cheng Ning Zhang ◽  
Shuo Zhang ◽  
Xiao Hua Wu
Keyword(s):  
Dynamic Model ◽  
Control Strategy ◽  
Control Method ◽  
Coordinated Control ◽  
Drive System ◽  
Simulation Platform ◽  
City Bus ◽  
Working Principle ◽  
Simulation Results

A novel drive system the Dual Motors Coupling Propulsion (DMCP) for battery electric buses was proposed, and its structure and working principle were introduced. For the power and comfort performance of the vehicle, the control method of the motors and the coordinated control strategy of the DMCP were developed. The co-simulation platform of AMESim and Simulink was established, based on which the dynamic model of the vehicle equipped the DMCP was built. The simulation results show that the DMCP runs smoothly in the Chinese typical city bus driving schedule. This indicates that the control strategy can manipulate the DMCP to drive the bus powerfully and smoothly. This has laid the foundation of the further research of the DMCP.

Study on a Control Method Used in the Semi-Active Suspension

2011 ◽  
Vol 128-129 ◽  
pp. 1025-1030
Author(s):  
Yun Tang Zhao ◽  
Si Zhong Chen ◽  
Zhan Zong Feng
Keyword(s):  
Control Strategy ◽  
Ride Comfort ◽  
Control Method ◽  
Active Suspension ◽  
The Other ◽  
Isolation Effect ◽  
Suspension Spring ◽  
Simulation Results ◽  
Active Damper ◽  
The Ideal

A new control method used in the semi-active suspension is studied. The force generated by the semi-active damper can be divided into two parts, one is the uncontrollable force, and the other is the controllable force. In order to make the sprung mass have the ideal isolation effect, the controllable force should be equal to the sum of the uncontrollable force and the force generated by the suspension spring. But the controllable force is limited by many constraints. Therefore, the control strategy can be concluded. The simulation results show that the ride comfort and handling stability are both improved by the control method.

AUV’s Executer Fault-Tolerant Control Based on ADRC

2014 ◽  
Vol 1006-1007 ◽  
pp. 581-585 ◽  
Author(s):  
Lei Wan ◽  
Ying Hao Zhang ◽  
Yu Shan Sun ◽  
Yue Ming Li
Keyword(s):  
Control Strategy ◽  
Pid Control ◽  
Disturbance Rejection ◽  
Control Method ◽  
Fault Tolerant ◽  
Fault Tolerant Control ◽  
Active Disturbance Rejection ◽  
Disturbance Rejection Control ◽  
Simulation Results ◽  
The One

An autonomous under vehicle (AUV) should have the ability of self-saving and finishing the certain targets when faults occur, which means that an AUV must have the ability of fault-tolerant control. In order to make it possible, one AUV’s fault-tolerant control strategy is made, which is based on the active disturbance rejection control (ADRC). In this paper, the control method in normal and the one in fault are offered respectively. Besides that, one simulation compared with PID control is made. The simulation results show the AUV’s fault-tolerant control strategy based on ADRC can achieve the goal and has better control results to restrain the shock, overshoot and other phenomena caused by disturbance than the strategy based on PID.

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