Force-based cooperative handling and lay-up of deformable materials: Mechatronic design, modeling, and control of a demonstrator

Mechatronics ◽  
2017 ◽  
Vol 47 ◽  
pp. 246-261 ◽  
Author(s):  
Stefan Flixeder ◽  
Tobias Glück ◽  
Andreas Kugi
Keyword(s):  
Modeling And Control ◽  
Mechatronic Design ◽  
Deformable Materials ◽  
And Control

Modeling and Control for Plant Dynamics Based on Reinforcement Learning

2009 ◽  
Vol 129 (4) ◽  
pp. 363-367
Author(s):  
Tomoyuki Maeda ◽  
Makishi Nakayama ◽  
Hiroshi Narazaki ◽  
Akira Kitamura
Keyword(s):  
Reinforcement Learning ◽  
Modeling And Control ◽  
Plant Dynamics ◽  
And Control

MODELING AND CONTROL OF HORIZONTAL FLEXIBLE PLATE USING PID-CS CONTROLLER

2019 ◽  
Vol 42 (4) ◽  
pp. 138-142
Author(s):  
Mohammed Jawad Mohammed ◽  
Majida Khalil Ahmed ◽  
Basma Abdullah Abbas
Keyword(s):  
Flexible Plate ◽  
Modeling And Control ◽  
And Control

An Efficient Approach for Modeling and Control of a Quadrotor

2016 ◽  
Vol 4 (2) ◽  
pp. 1-16
Author(s):  
Ahmed S. Khusheef
Keyword(s):  
Pid Control ◽  
Control Method ◽  
Mechanical Design ◽  
Loop Control ◽  
Modeling And Control ◽  
Loop Control System ◽  
And Control ◽  
Close Loop Control ◽  
Close Loop Control System ◽  
Made In

 A quadrotor is a four-rotor aircraft capable of vertical take-off and landing, hovering, forward flight, and having great maneuverability. Its platform can be made in a small size make it convenient for indoor applications as well as for outdoor uses. In model there are four input forces that are essentially the thrust provided by each propeller attached to each motor with a fixed angle. The quadrotor is basically considered an unstable system because of the aerodynamic effects; consequently, a close-loop control system is required to achieve stability and autonomy. Such system must enable the quadrotor to reach the desired attitude as fast as possible without any steady state error. In this paper, an optimal controller is designed based on a Proportional Integral Derivative (PID) control method to obtain stability in flying the quadrotor. The dynamic model of this vehicle will be also explained by using Euler-Newton method. The mechanical design was performed along with the design of the controlling algorithm. Matlab Simulink was used to test and analyze the performance of the proposed control strategy. The experimental results on the quadrotor demonstrated the effectiveness of the methodology used.

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