Real time parameter estimation for reconfigurable control of unstable aircraft

Kamali, C and Pashilkar, AA and Raol, JR (2007) Real time parameter estimation for reconfigurable control of unstable aircraft. Defence Science Journal. pp. 341-352.

Full text not available from this repository.


The real time open loop parameter estimation of unstable/augmented aircraft is very essential for reconfigurable/adaptive control. This paper describes two parameter estimation algorithms that are based on the equation error minimization principle. One is the recently developed, well-established recursive DGT technique in frequency domain. The other is an application of RLS in equation error minimization concept, applied to unstable/augmented aircraft parameter estimation. The RLS technique reported in these paper is implemented, for the first time, by a methodology that is analogous to the recursive DFT technique.

Item Type: Article
Uncontrolled Keywords: Real-time parameter estimation;Adaptive/reconfigurable control; Equation error;Discrete fourier transform;Recursive least squares;Digital filtering
Subjects: AERONAUTICS > Aircraft Stability and Control
Depositing User: M/S ICAST NAL
Date Deposited: 26 Feb 2008
Last Modified: 24 May 2010 04:25

Actions (login required)

View Item View Item