A method for designing multiple inputs for real-time dynamic system identification in the frequency domain was developed and demonstrated. The designed inputs are mutually orthogonal in both the time and frequency domains, with reduced peak factors to provide good information content for relatively small amplitude excursions. The inputs are designed for selected frequency ranges, and therefore do not require a priori models. The experiment design approach was applied to identify linear dynamic models for the F-15 ACTIVE aircraft, which has multiple control effectors
M.Ing. (Electrical and Electronic Engineering)This treatise presents an investigation into the appli...
M.Ing. (Electrical and Electronic Engineering)This treatise presents an investigation into the appli...
grantor: University of TorontoIn this thesis, system identification using the Frequency Sa...
A method for real-time estimation of parameters in a linear dynamic state space model was developed ...
A method is proposed and studied whereby the system identification cycle consisting of experiment de...
With the demand for more advanced fighter aircraft, relying on unstable flight mechanical characteri...
With the demand for more advanced fighter aircraft, relying on unstable flight mechanical characteri...
With the demand for more advanced fighter aircraft, relying on unstable flight mechanical characteri...
A method is proposed and studied whereby the system identification cycle consisting of experiment de...
A new technique was developed for designing optimal flight test inputs for aircraft parameter estima...
Practical aspects of the frequency-domain approach for aircraft system identification are explained ...
A flight test campaign for system identification is a time and cost consuming task. Models derived f...
Presented at the AIAA Atmospheric Flight Mechanics, Chicago, IL, August, 2009.In-flight identificati...
A flight test campaign for system identification is a costly and time-consuming task. Models derived...
A flight test campaign for system identification is a costly and time-consuming task. Models derived...
M.Ing. (Electrical and Electronic Engineering)This treatise presents an investigation into the appli...
M.Ing. (Electrical and Electronic Engineering)This treatise presents an investigation into the appli...
grantor: University of TorontoIn this thesis, system identification using the Frequency Sa...
A method for real-time estimation of parameters in a linear dynamic state space model was developed ...
A method is proposed and studied whereby the system identification cycle consisting of experiment de...
With the demand for more advanced fighter aircraft, relying on unstable flight mechanical characteri...
With the demand for more advanced fighter aircraft, relying on unstable flight mechanical characteri...
With the demand for more advanced fighter aircraft, relying on unstable flight mechanical characteri...
A method is proposed and studied whereby the system identification cycle consisting of experiment de...
A new technique was developed for designing optimal flight test inputs for aircraft parameter estima...
Practical aspects of the frequency-domain approach for aircraft system identification are explained ...
A flight test campaign for system identification is a time and cost consuming task. Models derived f...
Presented at the AIAA Atmospheric Flight Mechanics, Chicago, IL, August, 2009.In-flight identificati...
A flight test campaign for system identification is a costly and time-consuming task. Models derived...
A flight test campaign for system identification is a costly and time-consuming task. Models derived...
M.Ing. (Electrical and Electronic Engineering)This treatise presents an investigation into the appli...
M.Ing. (Electrical and Electronic Engineering)This treatise presents an investigation into the appli...
grantor: University of TorontoIn this thesis, system identification using the Frequency Sa...