Applications of unmanned small scaled helicopters are increasing recently because of their compactness in size and their ability to maneuver in hazardous environments. PUC-FLY is a small scale unmanned coaxial helicopter engineered at Purdue University Calumet. In this research, the flight dynamics of the helicopter is derived based on mathematical modeling for analyzing it behavior and for control design. This model is validated with a second model developed based on SimMechanics, which is a MATLAB toolbox. Furthermore, a significant part of the PUC-FLY is the sensor onboard, which provides the vehicles six Degree of Freedom (DOF) self-motion data. It consist a tri-axis gyroscope and accelerometer which provide the position and attitude of...
This paper describes helicopter model development work which will be used in the next stage of a res...
This paper discusses ongoing work being performed at the Naval Postgraduate School to develop a rota...
This paper aims to build an accurate mathematical model which is necessary for control design and at...
Unmanned Aerial Vehicles (UAVs) currently represent one of the most dynamic research areas for contr...
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...
Micro Coaxial Helicopter with compact size and vertical takeoff ability offers a good Micro Aerial V...
The focus of this thesis is the development of a generic small-scale unmanned helicopter model and a...
Micro Coaxial Helicopter with compact size and vertical takeoff ability offers a good Micro Aerial V...
The main characteristic attribute of the rotorcraft is the use of rotary wings to produce the thrust...
The aim of this research project is to develop an autopilot system that enables the helicopter model...
Abstract:- Helicopters are strongly coupled, multivariate, time-delay nonlinear plants. The design o...
UnrestrictedResearch on unmanned aerial vehicles is motivated by applications where human interventi...
Unmanned aerial vehicles (UAVs) have been more and more widely used not only in military areas but a...
Dissertation (Ph.D.)--University of Kansas, Aerospace Engineering, 2007.There has been a significant...
This paper describes helicopter model development work which will be used in the next stage of a res...
This paper discusses ongoing work being performed at the Naval Postgraduate School to develop a rota...
This paper aims to build an accurate mathematical model which is necessary for control design and at...
Unmanned Aerial Vehicles (UAVs) currently represent one of the most dynamic research areas for contr...
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...
Micro Coaxial Helicopter with compact size and vertical takeoff ability offers a good Micro Aerial V...
The focus of this thesis is the development of a generic small-scale unmanned helicopter model and a...
Micro Coaxial Helicopter with compact size and vertical takeoff ability offers a good Micro Aerial V...
The main characteristic attribute of the rotorcraft is the use of rotary wings to produce the thrust...
The aim of this research project is to develop an autopilot system that enables the helicopter model...
Abstract:- Helicopters are strongly coupled, multivariate, time-delay nonlinear plants. The design o...
UnrestrictedResearch on unmanned aerial vehicles is motivated by applications where human interventi...
Unmanned aerial vehicles (UAVs) have been more and more widely used not only in military areas but a...
Dissertation (Ph.D.)--University of Kansas, Aerospace Engineering, 2007.There has been a significant...
This paper describes helicopter model development work which will be used in the next stage of a res...
This paper discusses ongoing work being performed at the Naval Postgraduate School to develop a rota...
This paper aims to build an accurate mathematical model which is necessary for control design and at...