In this paper, we consider the problem of estimating the parameters in mathematical models of complex systems from experimental observations; the methods and procedures that we develop are general, but in this work we make specific reference to the problem of parameter estimation for multibody-based rotorcraft vehicle models from flight test data. We consider methods that are applicable to unstable systems, since rotorcraft vehicles are typically unstable at least in certain flight regimes. Unstable vehicles must be operated in closed-loop, and this must be explicitly accounted for when formulating parameter estimation methods. We describe two alternative classes of methods in the time domain, namely, the recursive filtering and the batch o...
This valuable volume offers a systematic approach to flight vehicle system identification and covers...
This article presents an integrated approach for the parameter identification of a small-scale unman...
Mixed estimation is presented as an approach to parameter estimation of unstable/augmented aircraft ...
In this paper, we consider the problem of estimating the parameters in mathematical models of comple...
In this paper, we consider the problem of parameter estimation from flight test data for rotorcraft ...
In this document, we consider the problem of parameter estimation from flight test data for rotorcra...
This work presents a method for estimating the model parameters of multi-rotor unmanned aerial vehic...
n this work, we explore time-domain parameter identification approaches to generate reduced models o...
Vehicle characteristics have a significant impact on handling, stability, and rollover propensity. T...
Parameter estimation method using an extended Kalman Filter Fast parameter estimation is a non-trivi...
This paper investigates the problem of estimating parameters in a state-space helicopter dynamical m...
Current frequency-domain system identification methods require an open-loop experiment design for da...
In this paper the analysis and results of recursive mixed estimation technique for parameter estimat...
This paper investigates the problem of estimating parameters in a state-space helicopter dynamical m...
As multi-rotor vehicles become integrated into the national airspace for applications such as packag...
This valuable volume offers a systematic approach to flight vehicle system identification and covers...
This article presents an integrated approach for the parameter identification of a small-scale unman...
Mixed estimation is presented as an approach to parameter estimation of unstable/augmented aircraft ...
In this paper, we consider the problem of estimating the parameters in mathematical models of comple...
In this paper, we consider the problem of parameter estimation from flight test data for rotorcraft ...
In this document, we consider the problem of parameter estimation from flight test data for rotorcra...
This work presents a method for estimating the model parameters of multi-rotor unmanned aerial vehic...
n this work, we explore time-domain parameter identification approaches to generate reduced models o...
Vehicle characteristics have a significant impact on handling, stability, and rollover propensity. T...
Parameter estimation method using an extended Kalman Filter Fast parameter estimation is a non-trivi...
This paper investigates the problem of estimating parameters in a state-space helicopter dynamical m...
Current frequency-domain system identification methods require an open-loop experiment design for da...
In this paper the analysis and results of recursive mixed estimation technique for parameter estimat...
This paper investigates the problem of estimating parameters in a state-space helicopter dynamical m...
As multi-rotor vehicles become integrated into the national airspace for applications such as packag...
This valuable volume offers a systematic approach to flight vehicle system identification and covers...
This article presents an integrated approach for the parameter identification of a small-scale unman...
Mixed estimation is presented as an approach to parameter estimation of unstable/augmented aircraft ...