Time domain system identification methods are employed to identify an extended linear model of a VTOL UAV around the hover domain using only noisy sensor measurements and recorded pilot inputs. The feasibility of employing principally time domain methods for system identification of miniature UAVs coupled with state-of-the-art sensors is demonstrated. The identified model is verified by testing against real flight data not used in the modeling process
In this paper, a semi-decoupled state space model of a small-size helicopter is developed for hoveri...
Modelling of innovative aircraft such as unmanned air vehicles (UAVs), X-wing, tilt body and delta-w...
Small low-cost unmanned aerial vehicles (UAVs) provide greater possibilities for personal scientific...
This article presents an integrated approach for the parameter identification of a small-scale unman...
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 aims to build an accurate mathematical model which is necessary for control design and at...
This paper presents the results, achieved at the Aerospace Engineering Department Laboratories of th...
System identification of an Unmanned Aerial Vehicle (UAV), to acquire its mathematical model, is a s...
This paper is focused on the model identification of a Micro Air Vehicle (MAV) in straight steady fl...
The unmanned helicopter Skeldar relies on model based control to per form its tasks. System identif...
Modelling of innovative aircraft such as unmanned air vehicles (UAVs), X-wing, tilt body and delta-w...
This paper illustrates a non-linear model for the dynamic simulation of small-scale helicopter and t...
The problem of rotorcraft system identification is considered and a novel, two-step technique is pro...
The availability of accurate models for helicopter aeromechanics is becoming more and more important...
In this paper, a semi-decoupled state space model of a small-size helicopter is developed for hoveri...
Modelling of innovative aircraft such as unmanned air vehicles (UAVs), X-wing, tilt body and delta-w...
Small low-cost unmanned aerial vehicles (UAVs) provide greater possibilities for personal scientific...
This article presents an integrated approach for the parameter identification of a small-scale unman...
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 aims to build an accurate mathematical model which is necessary for control design and at...
This paper presents the results, achieved at the Aerospace Engineering Department Laboratories of th...
System identification of an Unmanned Aerial Vehicle (UAV), to acquire its mathematical model, is a s...
This paper is focused on the model identification of a Micro Air Vehicle (MAV) in straight steady fl...
The unmanned helicopter Skeldar relies on model based control to per form its tasks. System identif...
Modelling of innovative aircraft such as unmanned air vehicles (UAVs), X-wing, tilt body and delta-w...
This paper illustrates a non-linear model for the dynamic simulation of small-scale helicopter and t...
The problem of rotorcraft system identification is considered and a novel, two-step technique is pro...
The availability of accurate models for helicopter aeromechanics is becoming more and more important...
In this paper, a semi-decoupled state space model of a small-size helicopter is developed for hoveri...
Modelling of innovative aircraft such as unmanned air vehicles (UAVs), X-wing, tilt body and delta-w...
Small low-cost unmanned aerial vehicles (UAVs) provide greater possibilities for personal scientific...