92 p.Guidance of an autonomous helicopter requires transforming a predened flight schedule, described as a series of discrete points, in a continuous smooth trajectory. A smooth flight schedule reduces the control system effort and decreases transients originated by direction and flight mode changes. Differently from airplanes, helicopter flight cannot be described only by position changes but also special flight mode changes (e.g. takeoff to hover). Reduced transients and control effort are dependent on the continuity of the planned three dimensional path, smooth velocity transitions and adequate management of mode transitions.Contenido parcial: Research contribution and methodology -- The small helicopter dynamic model -- Trajectory smoo...
In the last decades, research efforts related to Unmanned Aerial Vehicles (UAV) have grown substanti...
Published in Journal of Guidance Control and Dynamics, Vol. 28, No. 3, May–June 2005.Presented as P...
In this paper we describe the control logic that enabled a small-scale unmanned helicopter to execut...
This work is centered in the definition of a transition management system for a small autonomous hel...
The design of a high-performance guidance and control system for a small-scale helicopterUnmanned Ae...
Thesis (Ph. D.)--Massachusetts Institute of Technology, Dept. of Aeronautics and Astronautics, 2003....
Our research objective consists in developing a, model-based, automatic safety recovery system, for ...
New research activities on DLRs EC135 ACT/FHS research helicopter has led to new challenges for the ...
The nonlinear set of equations which represents helicopter motion are linearized about a prescribed ...
The main characteristic attribute of the rotorcraft is the use of rotary wings to produce the thrust...
This thesis explore the development of models for the simulation of flight and control laws for a Ro...
The objective of this paper is to present general techniques for simulating helicopter flight trajec...
University of Pisa is performing a research finalized to develop Rotary Unmanned Aerial Vehicles (RU...
[EN] This paper presents a review of the state of the art on modelling and control of autonomous hel...
University of Pisa is performing a research finalized to develop Rotary Unmanned Aerial Vehicles (RU...
In the last decades, research efforts related to Unmanned Aerial Vehicles (UAV) have grown substanti...
Published in Journal of Guidance Control and Dynamics, Vol. 28, No. 3, May–June 2005.Presented as P...
In this paper we describe the control logic that enabled a small-scale unmanned helicopter to execut...
This work is centered in the definition of a transition management system for a small autonomous hel...
The design of a high-performance guidance and control system for a small-scale helicopterUnmanned Ae...
Thesis (Ph. D.)--Massachusetts Institute of Technology, Dept. of Aeronautics and Astronautics, 2003....
Our research objective consists in developing a, model-based, automatic safety recovery system, for ...
New research activities on DLRs EC135 ACT/FHS research helicopter has led to new challenges for the ...
The nonlinear set of equations which represents helicopter motion are linearized about a prescribed ...
The main characteristic attribute of the rotorcraft is the use of rotary wings to produce the thrust...
This thesis explore the development of models for the simulation of flight and control laws for a Ro...
The objective of this paper is to present general techniques for simulating helicopter flight trajec...
University of Pisa is performing a research finalized to develop Rotary Unmanned Aerial Vehicles (RU...
[EN] This paper presents a review of the state of the art on modelling and control of autonomous hel...
University of Pisa is performing a research finalized to develop Rotary Unmanned Aerial Vehicles (RU...
In the last decades, research efforts related to Unmanned Aerial Vehicles (UAV) have grown substanti...
Published in Journal of Guidance Control and Dynamics, Vol. 28, No. 3, May–June 2005.Presented as P...
In this paper we describe the control logic that enabled a small-scale unmanned helicopter to execut...