In this paper, we formulate the hybrid dynamic of unmanned small scale helicopter (Yamaha R-50) as piecewise affine (PWA) model and transform it into equivalent mixed logical dynamic (MLD) model using hybrid system description language (HYSDEL) integrated with hybrid toolbox for MATLAB. This hybrid model is triggered by the location of this unmanned aerial vehicle (UAV) which has two modes. By using the MLD model, we design the controller using model predictive control (MPC) to calculate the optimal control action so that this UAV flights and tracks a trajectory. Finally, we simulate this UAV and its controller to track a rectangular trajectory. From the simulation results, this unmanned small scale helicopter follows given trajectory very ...
In this paper, we propose a hybrid modelling and control design scheme for an unmanned helicopter. T...
The main characteristic attribute of the rotorcraft is the use of rotary wings to produce the thrust...
Designing autonomous flight control system for a mini scale helicopter is very challenging due to th...
Abstract:- Helicopters are strongly coupled, multivariate, time-delay nonlinear plants. The design o...
Purpose - The purpose of this paper is to investigate the feasibility of controlling a small-scale h...
Kinematical and dynamical equations of a small scale unmanned helicoper are presented in the paper. ...
The Unmanned Air Vehicles (UAVs) are being integrated into our society at an increasing rate. The am...
This paper proposes a hierachical hybrid MPC approach to design feedback control functions for stabi...
M.Ing.Linear control system theory is well developed and has lead to a number of control system type...
Abstract. In this paper we present a new control approach for a quadrotor mini-helicopter using the ...
The design of a high-performance guidance and control system for a small-scale helicopterUnmanned Ae...
Dieser Beitrag ist mit Zustimmung des Rechteinhabers aufgrund einer (DFG geförderten) Allianz- bzw. ...
Our research objective consists in developing a, model-based, automatic safety recovery system, for ...
The focus of this thesis is the development of a generic small-scale unmanned helicopter model and a...
In this paper, the robust hybrid control design is investigated for a small scale helicopter flying ...
In this paper, we propose a hybrid modelling and control design scheme for an unmanned helicopter. T...
The main characteristic attribute of the rotorcraft is the use of rotary wings to produce the thrust...
Designing autonomous flight control system for a mini scale helicopter is very challenging due to th...
Abstract:- Helicopters are strongly coupled, multivariate, time-delay nonlinear plants. The design o...
Purpose - The purpose of this paper is to investigate the feasibility of controlling a small-scale h...
Kinematical and dynamical equations of a small scale unmanned helicoper are presented in the paper. ...
The Unmanned Air Vehicles (UAVs) are being integrated into our society at an increasing rate. The am...
This paper proposes a hierachical hybrid MPC approach to design feedback control functions for stabi...
M.Ing.Linear control system theory is well developed and has lead to a number of control system type...
Abstract. In this paper we present a new control approach for a quadrotor mini-helicopter using the ...
The design of a high-performance guidance and control system for a small-scale helicopterUnmanned Ae...
Dieser Beitrag ist mit Zustimmung des Rechteinhabers aufgrund einer (DFG geförderten) Allianz- bzw. ...
Our research objective consists in developing a, model-based, automatic safety recovery system, for ...
The focus of this thesis is the development of a generic small-scale unmanned helicopter model and a...
In this paper, the robust hybrid control design is investigated for a small scale helicopter flying ...
In this paper, we propose a hybrid modelling and control design scheme for an unmanned helicopter. T...
The main characteristic attribute of the rotorcraft is the use of rotary wings to produce the thrust...
Designing autonomous flight control system for a mini scale helicopter is very challenging due to th...