Masteroppgave i mekatronikk MAS500 2013 – Universitetet i Agder, GrimstadDevelopment of a new approach to the multicopter segment of the Unmanned Areal Vehicle (UAV) family is presented. The system is designed on a T-shaped tricopter platform with ability to tilt all three motors, hereby defined as Tilt Rotor Tricopter (TRT). The highly coupled nonlinear system is investigated through the mathematical model, and verified by simulations. Linearization of the system has been achieved around hovering conditions, and represented in the state-space environment. The Linear Quadratic Regulator (LQR) has been implemented on the physical system, achieving controllable flight. As the prestudy discovered no identical platforms to the TRT, we ar...
With multicopters finding more and more application in various fields, the study of different config...
This article deals with the problem of attitude control of multicopters. At first the basic properti...
This paper outlines the dynamic modelling as well as the attitude and altitude control of a rotary b...
Development of a new approach to the multicopter segment of the Unmanned Areal Vehicle (UAV) family ...
This paper presents our flight control development for the University of Glasgow Singapre (UGS) tilt...
In the last decade, with the continuous development of Drones or Unmanned Aerial Vehicles (UAVs), a ...
Research on the tri-rotor aerial robot is due to extra efficiency over other UAV’s regarding stabili...
The design, dynamics, and control allocation of tri-rotor unmanned aerial vehicles (UAVs) are introd...
In this paper, design, dynamics and control allocation of Tri-Rotor UAV are introduced. Tri-Rotor UA...
The main thematic of this paper is controlling the main manoeuvers of a tilt rotor UAV airplane in s...
Tri-rotor UAVs are more efficient compared to quadrotors in regard to the size and power requirement...
This thesis focuses on Model Reference Adaptive Control (MRAC) and its application to a tilt-rotor q...
Multi-directional aerial platforms can fly in almost any orientation and direction, often maneuverin...
The quadrotor is a 200 g MAV with rapid-prototyped rotors that are driven by four brushless electric...
Unmanned Aerial Vehicle (UAV) has received a growing attention for the last few years. In terms of c...
With multicopters finding more and more application in various fields, the study of different config...
This article deals with the problem of attitude control of multicopters. At first the basic properti...
This paper outlines the dynamic modelling as well as the attitude and altitude control of a rotary b...
Development of a new approach to the multicopter segment of the Unmanned Areal Vehicle (UAV) family ...
This paper presents our flight control development for the University of Glasgow Singapre (UGS) tilt...
In the last decade, with the continuous development of Drones or Unmanned Aerial Vehicles (UAVs), a ...
Research on the tri-rotor aerial robot is due to extra efficiency over other UAV’s regarding stabili...
The design, dynamics, and control allocation of tri-rotor unmanned aerial vehicles (UAVs) are introd...
In this paper, design, dynamics and control allocation of Tri-Rotor UAV are introduced. Tri-Rotor UA...
The main thematic of this paper is controlling the main manoeuvers of a tilt rotor UAV airplane in s...
Tri-rotor UAVs are more efficient compared to quadrotors in regard to the size and power requirement...
This thesis focuses on Model Reference Adaptive Control (MRAC) and its application to a tilt-rotor q...
Multi-directional aerial platforms can fly in almost any orientation and direction, often maneuverin...
The quadrotor is a 200 g MAV with rapid-prototyped rotors that are driven by four brushless electric...
Unmanned Aerial Vehicle (UAV) has received a growing attention for the last few years. In terms of c...
With multicopters finding more and more application in various fields, the study of different config...
This article deals with the problem of attitude control of multicopters. At first the basic properti...
This paper outlines the dynamic modelling as well as the attitude and altitude control of a rotary b...