This work is centered in the definition of a transition management system for a small autonomous helicopter based on trajectory smoothing and a finite state machine (FSM). A smooth flight schedule decreases transients originated by direction changes and flight mode transitions (e.g., horizontal flight to hover mode). Although previous works have presented trajectory generation and FSM oriented controls, no previous studies have mixed these approaches in a single framework together with speed transitions. The proposed methods are validated in simulation with a realistic dynamic model of a small helicopter. © 2009 Springer Science+Business Media B.V
MIng (Computer and Electronic Engineering), North-West University, Potchefstroom Campus, 2014The use...
University of Pisa is performing a research finalized to develop Rotary Unmanned Aerial Vehicles (RU...
The objective of this paper is to present general techniques for simulating helicopter flight trajec...
92 p.Guidance of an autonomous helicopter requires transforming a predened flight schedule, describe...
Our research objective consists in developing a, model-based, automatic safety recovery system, for ...
The design of a high-performance guidance and control system for a small-scale helicopterUnmanned Ae...
In this paper, the robust hybrid control design is investigated for a small scale helicopter flying ...
The main characteristic attribute of the rotorcraft is the use of rotary wings to produce the thrust...
In this paper we describe the control logic that enabled a small-scale unmanned helicopter to execut...
This thesis explore the development of models for the simulation of flight and control laws for a Ro...
Abstract. In this paper we describe the control logic that enabled a small-scale unmanned helicopter...
With the increased use of small unmanned systems, and even automated flight, safety is becoming an is...
This work focuses on the control law design for a class of aerial systems able to perform transition...
Thesis (Ph. D.)--Massachusetts Institute of Technology, Dept. of Aeronautics and Astronautics, 2003....
There has been a great deal of interest in the dynamics and control of unmanned helicopter robots si...
MIng (Computer and Electronic Engineering), North-West University, Potchefstroom Campus, 2014The use...
University of Pisa is performing a research finalized to develop Rotary Unmanned Aerial Vehicles (RU...
The objective of this paper is to present general techniques for simulating helicopter flight trajec...
92 p.Guidance of an autonomous helicopter requires transforming a predened flight schedule, describe...
Our research objective consists in developing a, model-based, automatic safety recovery system, for ...
The design of a high-performance guidance and control system for a small-scale helicopterUnmanned Ae...
In this paper, the robust hybrid control design is investigated for a small scale helicopter flying ...
The main characteristic attribute of the rotorcraft is the use of rotary wings to produce the thrust...
In this paper we describe the control logic that enabled a small-scale unmanned helicopter to execut...
This thesis explore the development of models for the simulation of flight and control laws for a Ro...
Abstract. In this paper we describe the control logic that enabled a small-scale unmanned helicopter...
With the increased use of small unmanned systems, and even automated flight, safety is becoming an is...
This work focuses on the control law design for a class of aerial systems able to perform transition...
Thesis (Ph. D.)--Massachusetts Institute of Technology, Dept. of Aeronautics and Astronautics, 2003....
There has been a great deal of interest in the dynamics and control of unmanned helicopter robots si...
MIng (Computer and Electronic Engineering), North-West University, Potchefstroom Campus, 2014The use...
University of Pisa is performing a research finalized to develop Rotary Unmanned Aerial Vehicles (RU...
The objective of this paper is to present general techniques for simulating helicopter flight trajec...