Autonomous Aerial Vehicles are playing a vital role in today’s world in many aspects. Specifically, in Military, Industrial Survey, data acquisition, Mineral exploration, Wildfire Monitoring, Traffic monitoring, Research Test Beds for the development of future technologies and much more. Helicopters are one of the most preferred categories when coming to a selection of the vehicle for any said application. The following thesis addresses the problem of designing a autonomous controller for a helicopter using H∞ control method. The procedure for the controller development involves model identification of the given system using the system identification techniques as the first step, wherein the mathematical model of the system is identified us...
In the last years UAV (Unmanned Aerial Vehicle) systems are become very actractive for various comme...
In this bachelor thesis, a nonlinear mathematical model simulation and linear controller design for ...
In this paper we will introduce the existing model of a helicopter for teaching dynamic systems. Lat...
This thesis presents the design of an autopilot capable of flying small unmanned helicopter with two...
MIng (Computer and Electronic Engineering), North-West University, Potchefstroom Campus, 2014The use...
The aim of this research project is to develop an autopilot system that enables the helicopter model...
The main characteristic attribute of the rotorcraft is the use of rotary wings to produce the thrust...
The focus of this thesis is the development of a generic small-scale unmanned helicopter model and a...
[EN] This paper presents a review of the state of the art on modelling and control of autonomous hel...
The deployment of unmanned aerial vehicles (UAV) in military applications increased the research abo...
This paper presents the results of attitude, velocity, heave and yaw controller design for an autono...
This paper present the results of attitude, velocity, heave and yaw controller design for UTM autono...
Abstract: A complete flight control scheme with detailed design methodology is proposed for an indoo...
Focus of this thesis was the improvement of the vertical flight performance of the small-scaled, unm...
UnrestrictedResearch on unmanned aerial vehicles is motivated by applications where human interventi...
In the last years UAV (Unmanned Aerial Vehicle) systems are become very actractive for various comme...
In this bachelor thesis, a nonlinear mathematical model simulation and linear controller design for ...
In this paper we will introduce the existing model of a helicopter for teaching dynamic systems. Lat...
This thesis presents the design of an autopilot capable of flying small unmanned helicopter with two...
MIng (Computer and Electronic Engineering), North-West University, Potchefstroom Campus, 2014The use...
The aim of this research project is to develop an autopilot system that enables the helicopter model...
The main characteristic attribute of the rotorcraft is the use of rotary wings to produce the thrust...
The focus of this thesis is the development of a generic small-scale unmanned helicopter model and a...
[EN] This paper presents a review of the state of the art on modelling and control of autonomous hel...
The deployment of unmanned aerial vehicles (UAV) in military applications increased the research abo...
This paper presents the results of attitude, velocity, heave and yaw controller design for an autono...
This paper present the results of attitude, velocity, heave and yaw controller design for UTM autono...
Abstract: A complete flight control scheme with detailed design methodology is proposed for an indoo...
Focus of this thesis was the improvement of the vertical flight performance of the small-scaled, unm...
UnrestrictedResearch on unmanned aerial vehicles is motivated by applications where human interventi...
In the last years UAV (Unmanned Aerial Vehicle) systems are become very actractive for various comme...
In this bachelor thesis, a nonlinear mathematical model simulation and linear controller design for ...
In this paper we will introduce the existing model of a helicopter for teaching dynamic systems. Lat...