Stability and accuracy analysis of power hardware in the loop system with different interface algorithms

2016 ◽  
Author(s):  
Tomoyuki Hatakeyama ◽  
Antonino Riccobono ◽  
Antonello Monti
Keyword(s):  
Loop System ◽  
Accuracy Analysis ◽  
Hardware In The Loop ◽  
Stability And Accuracy

scholarly journals Stability and Accuracy Analysis of Power Hardware-in-the-loop Simulation of Inductor Coupled Systems

2010 ◽  
Vol 130 (7) ◽  
pp. 902-912 ◽  
Author(s):  
Miao Hong ◽  
Yushi Miura ◽  
Toshifumi Ise ◽  
Yuki Sato ◽  
Toshinari Momose ◽  
...  
Keyword(s):  
Coupled Systems ◽  
Accuracy Analysis ◽  
Hardware In The Loop ◽  
Stability And Accuracy

scholarly journals Design and Analysis of a MPC-based Mechanical Hardware-in-the-Loop System for Full-Scale Wind Turbine System Test Benches

2017 ◽  
Vol 50 (1) ◽  
pp. 10985-10991 ◽  
Author(s):  
Christian Leisten ◽  
Uwe Jassmann ◽  
Johannes Balshüsemann ◽  
Mathias Hakenberg ◽  
Dirk Abel
Keyword(s):  
Wind Turbine ◽  
Full Scale ◽  
Loop System ◽  
Hardware In The Loop ◽  
Wind Turbine System

Development of a data-based hardware in the loop system for teaching control subjects

2021 ◽  
Author(s):  
Natalia Garavito Barreto ◽  
Jorge Eduardo Cote Ballesteros ◽  
Jhon Edisson Rodriguez Castellanos
Keyword(s):  
Loop System ◽  
Hardware In The Loop ◽  
Control Subjects

Simulation Precision Analysis of Line of Sight Between Bomb and Target on Hardware in the Loop System for Laser Guided Weapon Countermeasure

2015 ◽  
Vol 52 (1) ◽  
pp. 011202
Author(s):  
李慧 Li Hui ◽  
甘霖 Gan Lin ◽  
张文攀 Zhang Wenpan ◽  
梁巍巍 Liang Weiwei
Keyword(s):  
Loop System ◽  
Line Of Sight ◽  
Hardware In The Loop ◽  
Precision Analysis

scholarly journals Research on design method of double-loop electric servo loading system with high-frequency band based on H∞ control strategy

2020 ◽  
pp. 002029402096213
Author(s):  
Yang Shui ◽  
Jianli Wei ◽  
Jie Yan
Keyword(s):  
Frequency Band ◽  
Loop System ◽  
Aerodynamic Load ◽  
Double Loop ◽  
Hardware In The Loop ◽  
Load Spectrum ◽  
Electric Loading ◽  
Technical Requirements ◽  
Loading System ◽  
High Dynamic

In the hardware-in-the-loop simulation, the goal of electric loading is to realize the accurate tracking of the torque signal and test the performance of the aircraft actuator system. For some high dynamic aircraft, it is necessary to reduce the influence of the surplus torque to increase the system frequency band. This paper introduces a new electric loading system which adopts a double-loop servo motor as the torque loading mechanism. It applies two loops to track the position of the rudder and the aerodynamic load spectrum respectively. For the purpose of reducing the disturbance between two loops of the scheme, a two-DOF H∞ robust controller is designed, which improves the robustness of the system effectively. The simulation results show that the new system increases the upper limit of 25 Hz frequency band of the traditional single-loop system with PID control to the maximum of 40 Hz. The double-loop system thereby meets the technical requirements of the hardware-in-the-loop simulation experiment for high dynamic aircrafts.

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