Kamali, C and Bhogle, JR and Pashilkar, AA (1996) Implementation of real-time parameter estimation in LabVIEW and DSP. Journal of Aerospace Science and Technologies . pp. 353-397.Full text not available from this repository.
This paper presents the results of real time aircraft parameter estimation technology in an aircrafi real time simulator. The equation error Recursive Least Squares (RLS) method is used for performing the parameter estimation. The RLS technique is successfully adapted for on-line parameter estimation y(t) Observation vector by a novel methodology that when measurements of state derivatives are not available. Subsequently, the algorithm is implemented in LabVIEW and in digitdl signal processor (DSP) hardware to demonstrate its suitability for further implementation at flight test centers and for on-board parameter estimation for aircraft.
|Item Type:||Journal Article|
|Uncontrolled Keywords:||Real-time parameter estimation;Equation error;Recursive least squares;Digital filtering|
|Subjects:||AERONAUTICS > Aircraft Stability and Control|
|Division/Department:||Flight Mechanics and Control Division, Other, Flight Mechanics and Control Division|
|Depositing User:||M/S ICAST NAL|
|Date Deposited:||24 Mar 2008|
|Last Modified:||24 May 2010 09:55|
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