Modeling, Control and Coordination of Helicopter Systems provides a comprehensive treatment of helicopter systems, ranging from related nonlinear flight dynamic modeling and stability analysis to advanced control design for single helicopter systems, and also covers issues related to the coordination and formation control of multiple helicopter systems to achieve high performance tasks. Ensuring stability in helicopter flight is a challenging problem for nonlinear control design and development. This book is a valuable reference on modeling, control and coordination of helicopter systems,providing readers with practical solutions for the problems that still plague helicopter system design and implementation. Readers will gain a complete pic...
This thesis presents the results of a study into the use of Hꝏ-optimization for the design of feedba...
In this thesis a dynamical model is developed for general six degrees of freedom quadrotor vehicle. ...
Abstract- Unmanned Aerial Vehicle become popular and very useful today. Unmanned Aerial Vehicle type...
The main characteristic attribute of the rotorcraft is the use of rotary wings to produce the thrust...
The helicopter is specific in regards to other traffictransportation means, not just by its structur...
This thesis is concerned with controller design for helicopter systems. The emphasis will be focused...
The concept of helicopter controllability is explained. A background study reviews helicopter devel...
[EN] This paper presents a review of the state of the art on modelling and control of autonomous hel...
The broad aim of the collaborative research programme between the Australian Defence Science Technol...
In this paper we will introduce the existing model of a helicopter for teaching dynamic systems. Lat...
The scope of this report is the development of a mathematical model and a control system for a three...
This paper presents the modelling and control of a laboratory helicopter system with MatLab. In this...
The paper will review the development and application of the mathematical modelling of the advanced ...
This project aims at designing an on-line controller in the form of a Multi Input\ud Multi Output Se...
Helicopter missions place strong demands on the precise control characteristics of aircraft, particu...
This thesis presents the results of a study into the use of Hꝏ-optimization for the design of feedba...
In this thesis a dynamical model is developed for general six degrees of freedom quadrotor vehicle. ...
Abstract- Unmanned Aerial Vehicle become popular and very useful today. Unmanned Aerial Vehicle type...
The main characteristic attribute of the rotorcraft is the use of rotary wings to produce the thrust...
The helicopter is specific in regards to other traffictransportation means, not just by its structur...
This thesis is concerned with controller design for helicopter systems. The emphasis will be focused...
The concept of helicopter controllability is explained. A background study reviews helicopter devel...
[EN] This paper presents a review of the state of the art on modelling and control of autonomous hel...
The broad aim of the collaborative research programme between the Australian Defence Science Technol...
In this paper we will introduce the existing model of a helicopter for teaching dynamic systems. Lat...
The scope of this report is the development of a mathematical model and a control system for a three...
This paper presents the modelling and control of a laboratory helicopter system with MatLab. In this...
The paper will review the development and application of the mathematical modelling of the advanced ...
This project aims at designing an on-line controller in the form of a Multi Input\ud Multi Output Se...
Helicopter missions place strong demands on the precise control characteristics of aircraft, particu...
This thesis presents the results of a study into the use of Hꝏ-optimization for the design of feedba...
In this thesis a dynamical model is developed for general six degrees of freedom quadrotor vehicle. ...
Abstract- Unmanned Aerial Vehicle become popular and very useful today. Unmanned Aerial Vehicle type...