Fuzzy logic controller (FLC) is a heuristic method by If-Then Rules which resembles human intelligence and it is a good method for designing Non-linear control systems. In this paper, an arbitrary helicopter model includes articulated manipulators has been simulated with Matlab SimMechanics toolbox. Due to the difficulties of modeling this complex system, a fuzzy controller with simple fuzzy rules has been designed for its yaw and roll angles in order to stabilize the helicopter while it is in the presence of disturbances or its manipulators are moving for a task. Results reveal that a simple FLC can appropriately control this system
This research focuses on travel angle control of a laboratory scale bench-top helicopter developed b...
In this paper the concept of Control Inertia is introduced and based on this concept, unexpectedly i...
The article is a continuation of research into a stabilization system for the Unmanned Aerial Vehicl...
<p>Fuzzy logic controller (FLC) is a heuristic method by If-Then Rules which resembles human intelli...
Helicopter instability represents a key issue in non-linear applications that should be addressed. A...
An assessment on flight control system of an aircraft system was done based on time response perform...
The flight control system of helicopter is difficult to control for their performance of high-order ...
Copyright © 2004-2006 Inderscience Enterprises LimitedIn this research, a fuzzy knowledge-base contr...
Summarization: In this paper the design process of a fuzzy logic based controller for a coaxial micr...
Bench-top helicopter with 3 Degree of freedom is developed by the Quanser Inc. It is a small-scale h...
©2006 IEEE. Personal use of this material is permitted. However, permission to reprint/republish thi...
A helicopter has nonlinear dynamics and it’s a multivariable system. A helicopter is an unstable pla...
In this research, the fuzzy control of the yaw angle of a model helicopter is studied, particularly,...
The studies in aerial vehicles modeling and control have been increased rapidly recently. This paper...
n this paper we present a new design method for the fight control of an autonomous quadrotor helicop...
This research focuses on travel angle control of a laboratory scale bench-top helicopter developed b...
In this paper the concept of Control Inertia is introduced and based on this concept, unexpectedly i...
The article is a continuation of research into a stabilization system for the Unmanned Aerial Vehicl...
<p>Fuzzy logic controller (FLC) is a heuristic method by If-Then Rules which resembles human intelli...
Helicopter instability represents a key issue in non-linear applications that should be addressed. A...
An assessment on flight control system of an aircraft system was done based on time response perform...
The flight control system of helicopter is difficult to control for their performance of high-order ...
Copyright © 2004-2006 Inderscience Enterprises LimitedIn this research, a fuzzy knowledge-base contr...
Summarization: In this paper the design process of a fuzzy logic based controller for a coaxial micr...
Bench-top helicopter with 3 Degree of freedom is developed by the Quanser Inc. It is a small-scale h...
©2006 IEEE. Personal use of this material is permitted. However, permission to reprint/republish thi...
A helicopter has nonlinear dynamics and it’s a multivariable system. A helicopter is an unstable pla...
In this research, the fuzzy control of the yaw angle of a model helicopter is studied, particularly,...
The studies in aerial vehicles modeling and control have been increased rapidly recently. This paper...
n this paper we present a new design method for the fight control of an autonomous quadrotor helicop...
This research focuses on travel angle control of a laboratory scale bench-top helicopter developed b...
In this paper the concept of Control Inertia is introduced and based on this concept, unexpectedly i...
The article is a continuation of research into a stabilization system for the Unmanned Aerial Vehicl...