n this work, we explore time-domain parameter identification approaches to generate reduced models of a comprehensive UH-60-like multibody model. Data required for the identification are gathered performing a few virtual experiments, in which the full system is perturbed about the hover condition, in either open-loop or closed-loop conditions. We validate the identified reduced models against a different set of experiments, discussing the main drawbacks of the employed methods. Moreover, we show some preliminary tracking results, where the comprehensive model is steered along a Category A continued take-off maneuver by a simple LQR controller synthesized from the identified models
Accurate dynamic modeling of helicopter aeromechanics is becoming increasingly important, as progres...
This paper introduces a new approach for the identification of linear state-space models of dynamica...
The problem of rotorcraft system identification is considered and a novel, two step technique is pro...
n this work, we explore time-domain parameter identification approaches to generate reduced models o...
As multi-rotor vehicles become integrated into the national airspace for applications such as packag...
The availability of accurate models for helicopter aeromechanics is becoming more and more important...
We describe a computational procedure for the simulation of maneuvers with comprehensive rotorcraft ...
Copyright © 2019 by the Vertical Flight Society. All rights reserved. The research reported in this ...
High fidelity rotorcraft flight simulation relies on the availability of a quality flight model that...
Current frequency-domain system identification methods require an open-loop experiment design for da...
The problem of rotorcraft system identification is considered and a novel, two-step technique is pro...
In this paper, we consider the problem of estimating the parameters in mathematical models of comple...
The availability of suitable methods for system identification from flight data of rotorcraft models...
High-fidelity rotorcraft flight simulation relies on the availability of a quality flight model that...
Accurate dynamic modeling of helicopter aeromechanics is becoming increasingly important, as progres...
This paper introduces a new approach for the identification of linear state-space models of dynamica...
The problem of rotorcraft system identification is considered and a novel, two step technique is pro...
n this work, we explore time-domain parameter identification approaches to generate reduced models o...
As multi-rotor vehicles become integrated into the national airspace for applications such as packag...
The availability of accurate models for helicopter aeromechanics is becoming more and more important...
We describe a computational procedure for the simulation of maneuvers with comprehensive rotorcraft ...
Copyright © 2019 by the Vertical Flight Society. All rights reserved. The research reported in this ...
High fidelity rotorcraft flight simulation relies on the availability of a quality flight model that...
Current frequency-domain system identification methods require an open-loop experiment design for da...
The problem of rotorcraft system identification is considered and a novel, two-step technique is pro...
In this paper, we consider the problem of estimating the parameters in mathematical models of comple...
The availability of suitable methods for system identification from flight data of rotorcraft models...
High-fidelity rotorcraft flight simulation relies on the availability of a quality flight model that...
Accurate dynamic modeling of helicopter aeromechanics is becoming increasingly important, as progres...
This paper introduces a new approach for the identification of linear state-space models of dynamica...
The problem of rotorcraft system identification is considered and a novel, two step technique is pro...