Twin Rotor Multi Input Multi Output (MIMO) System (TRMS) is a laboratory set-up design for which it has been used for control experiments, control theories developments, and applications of the autonomous helicopter. Fuzzy Logic Control (FLC) has been widely used with different control schemes to cope with control objectives of TRMS. In this work, Self Tuning Fuzzy PD-like Controller (STFPDC) is proposed to make the response of FLC more robust to the interactions and the non-linearity of the process in terms of less rising time, settling time and overshoot. Adaptive Neuro Fuzzy Inference System (ANFIS) based Fuzzy Subtractive Clustering Method (FSCM) was used to remodel the proposed STFPDC to achieve the control objectives on TRMS with less...
This paper presents a comparative study of fuzzy controller design for the twin rotor multi-input mu...
Artificial intelligence techniques, such as neural networks and fuzzy logic have shown promising r...
An assessment on flight control system of an aircraft system was done based on time response perform...
This work presents a self-tuning fuzzy PD controller for solving the control challenges of twin roto...
This study examines the modelling and control of a twin rotor multi-input multi-output (MIMO) system...
In this paper, Neuro-Fuzzy based Fuzzy Subtractive Clustering Method (FSCM) and Self Tuning Fuzzy PD...
A new multiple-input multiple-output (MIMO) proportional-integral-proportional-derivative (PIPD) typ...
The flight control system of helicopter is difficult to control for their performance of high-order ...
The flight control system of helicopter is difficult to control for their performance of high-order ...
This paper presents the designing of fuzzy logic co ntroller for a twin rotor multi-input-multi- o...
This paper presents the design of a Fuzzy PID controller (FPID) based on fuzzy logic with a PID stru...
[[abstract]]In this paper, a method to obtain the optimal parameters of PID(Proportional, Integral a...
Twin Rotor MIMO system (TRMS) is considered as a prototype model of Helicopter. The aim of studying ...
Twin Rotor MIMO System (TRMS) is a dynamic model with high non-linearity that resembles a helicopter...
Artificial intelligence techniques, such as neural networks and fuzzy logic have shown promising r...
This paper presents a comparative study of fuzzy controller design for the twin rotor multi-input mu...
Artificial intelligence techniques, such as neural networks and fuzzy logic have shown promising r...
An assessment on flight control system of an aircraft system was done based on time response perform...
This work presents a self-tuning fuzzy PD controller for solving the control challenges of twin roto...
This study examines the modelling and control of a twin rotor multi-input multi-output (MIMO) system...
In this paper, Neuro-Fuzzy based Fuzzy Subtractive Clustering Method (FSCM) and Self Tuning Fuzzy PD...
A new multiple-input multiple-output (MIMO) proportional-integral-proportional-derivative (PIPD) typ...
The flight control system of helicopter is difficult to control for their performance of high-order ...
The flight control system of helicopter is difficult to control for their performance of high-order ...
This paper presents the designing of fuzzy logic co ntroller for a twin rotor multi-input-multi- o...
This paper presents the design of a Fuzzy PID controller (FPID) based on fuzzy logic with a PID stru...
[[abstract]]In this paper, a method to obtain the optimal parameters of PID(Proportional, Integral a...
Twin Rotor MIMO system (TRMS) is considered as a prototype model of Helicopter. The aim of studying ...
Twin Rotor MIMO System (TRMS) is a dynamic model with high non-linearity that resembles a helicopter...
Artificial intelligence techniques, such as neural networks and fuzzy logic have shown promising r...
This paper presents a comparative study of fuzzy controller design for the twin rotor multi-input mu...
Artificial intelligence techniques, such as neural networks and fuzzy logic have shown promising r...
An assessment on flight control system of an aircraft system was done based on time response perform...