Disturbance Compensation and Control Algorithm with Application for Non-linear Twin Rotor MIMO System

2017 ◽  
pp. 428-435
Author(s):  
Alexey Margun ◽  
Igor Furtat ◽  
Dmitry Bazylev ◽  
Artem Kremlev
Keyword(s):  
Control Algorithm ◽  
Mimo System ◽  
Disturbance Compensation ◽  
Non Linear ◽  
Twin Rotor Mimo System ◽  
And Control ◽  
Twin Rotor

Adaptive Active Force Control Application to Twin Rotor Mimo System

2013 ◽  
Vol 393 ◽  
pp. 688-693 ◽  
Author(s):  
Hanif Ramli ◽  
Wahyu Kuntjoro ◽  
M.S. Meon ◽  
K.M Asraf K. Ishak
Keyword(s):  
Force Control ◽  
Control Algorithm ◽  
Mimo System ◽  
Active Force ◽  
Optimum Control ◽  
Active Force Control ◽  
Non Linear ◽  
Artificial Neural Network Ann ◽  
Twin Rotor Mimo System ◽  
Twin Rotor

This paper reports a current study on modeling and simulation of adaptive Active Force Control (AFC) based scheme embedded with an artificial neural network (ANN) and/or fuzzy logic (FL) in response manipulations of the twin rotor multi-input multi-output (MIMO) system (TRMS). TRMS is well known for its non-linear behaviour and common classical control scheme such as Proportional-Integral-Derivative (PID) would not be adequate to compensate disturbances. The disturbances in this case were as the results of non-linear external and internal parametric changes, namely angular momentum and couple reactions between the two axes of TRMS. The adaptive control algorithm was proposed in both pitch and yaw to generate an optimum control gain for both responses, simulated viz. MATLAB/SIMULINK software Package. The ANN and FL were integrated into the scheme and act as optimum control algorithm in catalyzing the performance of the TRMS. The results from hybrid conditions of PID-AFC, PID-AFC-ANN and PID-AFC-FL respectively were observed and analyzed. From performance evaluation, PID-AFC-FL scheme has demonstrated a potentially robust and effective manipulating capability in trajectory tracking.

scholarly journals H∞BASEDOBSERVER FOR DISTURBANCE COMPENSATION IN DECOUPLED TRMS USING LMI OPTIMIZATION

2014 ◽  
pp. 213-218
Author(s):  
LEKSHMI S ◽  
JEEVAMMA JACOB
Keyword(s):  
Disturbance Rejection ◽  
Control Method ◽  
Mimo System ◽  
Cost Effective ◽  
Laboratory Model ◽  
Disturbance Compensation ◽  
Lmi Optimization ◽  
Twin Rotor Mimo System ◽  
Model Inverse ◽  
Twin Rotor

Twin Rotor MIMO System is a laboratory model of helicopter. In this paper, the problem of disturbance rejection in TRMS is dealt with. Using disturbance observers, without any additional sensors is an attractive method to attenuate the effects of disturbances as they are highly cost effective. This method uses a simple form of DOBs, which does not need to solve the plant model inverse, and uses H∞control method using LMIs to design the Q-filter in the DOB. The estimation capability of DOB is verified using simulation results in frequency domain as well as in time domain.

scholarly journals Design and performance comparison of different adaptive control schemes for pitch angle control in a twin – rotor – MIMO – system

2019 ◽  
Vol 9 (5) ◽  
pp. 4114 ◽  
Author(s):  
Winston Netto ◽  
Rohan Lakhani ◽  
S. Meenatchi Sundaram
Keyword(s):  
Adaptive Control ◽  
Mimo System ◽  
Cross Coupling ◽  
Performance Comparison ◽  
Superior Performance ◽  
Main Rotor ◽  
Adaptive Schemes ◽  
Non Linear ◽  
Twin Rotor Mimo System ◽  
Twin Rotor

The Twin Rotor MIMO System is a higher order non-linear plant and is inherently unstable due to cross coupling between tail and main rotor. In this paper only the control of main rotor is considered which is non-linear and stable by using adaptive schemes. The control problem is to achieve perfect tracking for input reference signals while maintaining robustness and stability. Four adaptive schemes were implemented, two using Model Reference Adaptive Control under which MIT rule and Modified MIT rule are used. The other two using Adaptive Interaction, namely, Adaptive PID and Approximate Adaptive PID. It is observed that adaptive schemes fulfill all the three system performance requirements at the same time. Modified MIT rule was found to give superior performance in comparison to other controllers. Also Approximate Adaptive PID was able to stabilize the main rotor and cancel the effect of cross coupling between tail rotor and main rotor when operating simultaneously without the need for designing decouplers for the system. Thus the main rotor can be made independent from the state of the tail rotor by using Approximate Adaptive PID.

Quasi-LPV modeling, identification and control of a twin rotor MIMO system

2013 ◽  
Vol 21 (6) ◽  
pp. 829-846 ◽  
Author(s):  
Damiano Rotondo ◽  
Fatiha Nejjari ◽  
Vicenç Puig
Keyword(s):  
Mimo System ◽  
Twin Rotor Mimo System ◽  
And Control ◽  
Twin Rotor
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