Published in Journal of Guidance Control and Dynamics, 29(4):769-779, July, 2006.Small ducted fan autonomous vehicles have potential for several applications, especially for missions in urban environments. This paper discusses the use of dynamic inversion with neural network adaptation to provide an adaptive controller for the GTSpy, a small ducted fan autonomous vehicle based on the Micro Autonomous Systems' Helispy. This approach allows utilization of the entire low speed flight envelope with a relatively poorly understood vehicle. A simulator model is constructed from a force and moment analysis of the vehicle, allowing for a validation of the controller in preparation for flight testing. Data from flight testing of the system is ...
A small scale tri-rotor test bed with tilting propellers has been built to test flight control laws ...
This chapter deals with the control system development and flight test for an unconventional flight ...
In this paper, we present a neural adaptive back-stepping flight controller for a ducted fan UAV who...
Small ducted fan aerial unmanned aerial vehicles possess hover and vertical take-off and landing cap...
The design of autonomous navigation strategies for ducted fan unmanned aerial vehicleshas now become...
In this paper, we focus on the transition control of a ducted fan vertical take-off and landing (VTO...
Fixed-wing unmanned aerial vehicles (UAVs) with the ability to hover have significant potential for ...
AbstractThis paper presents a simple and useful modeling method to acquire a dynamics model of an ae...
none3This paper presents results relative to the prototyping, modelling and design of a control sys...
This paper deals with the development of a flight control scheme based on the Nonlinear Dynamic Inve...
This paper deals with the development of a flight control scheme based on the Nonlinear Dynamic Inve...
Linear systems can be used to adequatelymodel and control an aircraft in either ideal steady-level f...
Unmanned Aerial Vehicles are self-piloted or remotely piloted aircrafts that have the capacity to fl...
In this paper an experimental activity carried out at the University of Bologna regarding the develo...
The aerodynamic parameters of ducted fan micro aerial vehicles (MAVs) are difficult and expensive to...
A small scale tri-rotor test bed with tilting propellers has been built to test flight control laws ...
This chapter deals with the control system development and flight test for an unconventional flight ...
In this paper, we present a neural adaptive back-stepping flight controller for a ducted fan UAV who...
Small ducted fan aerial unmanned aerial vehicles possess hover and vertical take-off and landing cap...
The design of autonomous navigation strategies for ducted fan unmanned aerial vehicleshas now become...
In this paper, we focus on the transition control of a ducted fan vertical take-off and landing (VTO...
Fixed-wing unmanned aerial vehicles (UAVs) with the ability to hover have significant potential for ...
AbstractThis paper presents a simple and useful modeling method to acquire a dynamics model of an ae...
none3This paper presents results relative to the prototyping, modelling and design of a control sys...
This paper deals with the development of a flight control scheme based on the Nonlinear Dynamic Inve...
This paper deals with the development of a flight control scheme based on the Nonlinear Dynamic Inve...
Linear systems can be used to adequatelymodel and control an aircraft in either ideal steady-level f...
Unmanned Aerial Vehicles are self-piloted or remotely piloted aircrafts that have the capacity to fl...
In this paper an experimental activity carried out at the University of Bologna regarding the develo...
The aerodynamic parameters of ducted fan micro aerial vehicles (MAVs) are difficult and expensive to...
A small scale tri-rotor test bed with tilting propellers has been built to test flight control laws ...
This chapter deals with the control system development and flight test for an unconventional flight ...
In this paper, we present a neural adaptive back-stepping flight controller for a ducted fan UAV who...