Because most multivariable control methods are model-based, and the dynamic model for a particular small-scale helicopter which is simple enough to be practical for controller is not readily available, the identification of small-scale helicopter's dynamic model is a necessary part of any model-based control design. This paper describes the MOESP method which uses numerically robust computation tools applied in the model identification of a small-scale helicopter dynamics. The result of simulation shows this method is suitable for the dynamic identification of a small-scale helicopter
The focus of this thesis is the development of a generic small-scale unmanned helicopter model and a...
This paper aims to build an accurate mathematical model which is necessary for control design and at...
This paper explains how the method of system identification can be applied to a quadrotor helicopter...
This paper investigates the problem of helicopter dynamic modelling using time-domain system identif...
This paper investigates the problem of helicopter dynamic modelling using time-domain system identif...
Subspace identification is a powerful tool due to its well-understood techniques based on linear alg...
This article presents an integrated approach for the parameter identification of a small-scale unman...
Accurate dynamic modeling of helicopter aeromechanics is becoming increasingly important, as progres...
In this paper, a semi-decoupled state space model of a small-size helicopter is developed for hoveri...
In this paper, a semi-decoupled state-space model of a small-size helicopter is developed for hoveri...
This paper illustrates a non-linear model for the dynamic simulation of small-scale helicopter and t...
The success of model-based ight control law design for autonomous helicopter is largely dependent...
The paper presents a non-linear model for the dynamic simulation of small-scale helicopter and the a...
In this paper, a semi-decoupled state space model of a small-size helicopter is developed for hoveri...
This paper presents a method for characterising the primary dynamics of a rotary unmanned aerial veh...
The focus of this thesis is the development of a generic small-scale unmanned helicopter model and a...
This paper aims to build an accurate mathematical model which is necessary for control design and at...
This paper explains how the method of system identification can be applied to a quadrotor helicopter...
This paper investigates the problem of helicopter dynamic modelling using time-domain system identif...
This paper investigates the problem of helicopter dynamic modelling using time-domain system identif...
Subspace identification is a powerful tool due to its well-understood techniques based on linear alg...
This article presents an integrated approach for the parameter identification of a small-scale unman...
Accurate dynamic modeling of helicopter aeromechanics is becoming increasingly important, as progres...
In this paper, a semi-decoupled state space model of a small-size helicopter is developed for hoveri...
In this paper, a semi-decoupled state-space model of a small-size helicopter is developed for hoveri...
This paper illustrates a non-linear model for the dynamic simulation of small-scale helicopter and t...
The success of model-based ight control law design for autonomous helicopter is largely dependent...
The paper presents a non-linear model for the dynamic simulation of small-scale helicopter and the a...
In this paper, a semi-decoupled state space model of a small-size helicopter is developed for hoveri...
This paper presents a method for characterising the primary dynamics of a rotary unmanned aerial veh...
The focus of this thesis is the development of a generic small-scale unmanned helicopter model and a...
This paper aims to build an accurate mathematical model which is necessary for control design and at...
This paper explains how the method of system identification can be applied to a quadrotor helicopter...