Abstract. In this paper modelling and identification of a laboratory helicopter with the final aim to design a control system is presented. The CE 150 made by Humusoft is a laboratory helicopter designed for studying system dynamics and control engineering principles. First, the helicopter set-up is depicted. Next, theoretical and empyric modelling is systematically described. Identification of the necessary parameters is tackled and the results are presented. Finally, model validation is discussed and a simple control approach is proposed
This work deals with designing and testing of education model "Helicopter with two rotors". The firs...
This paper illustrates a non-linear model for the dynamic simulation of small-scale helicopter and t...
Control algorithms are at the heart of the stability and automatic flight capabilities of any aerial...
In this paper we will introduce the existing model of a helicopter for teaching dynamic systems. Lat...
This work explores two different approaches in the helicopter system (HUMUSOFT CE-150) identificat...
Abstract: This paper presents the modelling and control of a laboratory helicopter system with MatLa...
This paper presents the modelling and control of a laboratory helicopter system with MatLab. In this...
This thesis addresses rotorcraft system identification approaches and estimating the stability and c...
This paper presents a new mathematical model for a model-scale helicopter. Working from first princi...
Modelling a linear mathematical model of a radio controlled (RC) helicopter in hover is the main goa...
Autonomous Aerial Vehicles are playing a vital role in today’s world in many aspects. Specifically, ...
MIng (Computer and Electronic Engineering), North-West University, Potchefstroom Campus, 2014The use...
Helicopters are heavily coupled, unstable and their modeling is often a difficult nut to crack. This...
La stabilisation et l’automatisation du vol de tout véhicule aérien nécessite la mise en oeuvre d’al...
The focus of this thesis is the development of a generic small-scale unmanned helicopter model and a...
This work deals with designing and testing of education model "Helicopter with two rotors". The firs...
This paper illustrates a non-linear model for the dynamic simulation of small-scale helicopter and t...
Control algorithms are at the heart of the stability and automatic flight capabilities of any aerial...
In this paper we will introduce the existing model of a helicopter for teaching dynamic systems. Lat...
This work explores two different approaches in the helicopter system (HUMUSOFT CE-150) identificat...
Abstract: This paper presents the modelling and control of a laboratory helicopter system with MatLa...
This paper presents the modelling and control of a laboratory helicopter system with MatLab. In this...
This thesis addresses rotorcraft system identification approaches and estimating the stability and c...
This paper presents a new mathematical model for a model-scale helicopter. Working from first princi...
Modelling a linear mathematical model of a radio controlled (RC) helicopter in hover is the main goa...
Autonomous Aerial Vehicles are playing a vital role in today’s world in many aspects. Specifically, ...
MIng (Computer and Electronic Engineering), North-West University, Potchefstroom Campus, 2014The use...
Helicopters are heavily coupled, unstable and their modeling is often a difficult nut to crack. This...
La stabilisation et l’automatisation du vol de tout véhicule aérien nécessite la mise en oeuvre d’al...
The focus of this thesis is the development of a generic small-scale unmanned helicopter model and a...
This work deals with designing and testing of education model "Helicopter with two rotors". The firs...
This paper illustrates a non-linear model for the dynamic simulation of small-scale helicopter and t...
Control algorithms are at the heart of the stability and automatic flight capabilities of any aerial...