Ramamoorthy, P (1989) Extended Kalman Filter Algorithm (EKF). Technical Report. National Aerospace Laboratories, Bangalore, India.
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Abstract
An extended Kalman filter (EKF) algorithm is implemented on UNIVAC 1100/70. As an example, the longitudinal states, characterising the short period dynamics of an aircraft are obtained from noisy measured data.13; 13; This algorithm, with minor modifications and the incorporation of a stiff differential equation solution algorithm, could be implemented for extraction of stability and control derivatives from noisy flight test, data.
| Item Type: | Proj.Doc/Technical Report (Technical Report) |
|---|---|
| Uncontrolled Keywords: | Kalman filter;Estimation;Short period dynamics |
| Subjects: | AERONAUTICS > Aircraft Stability and Control |
| Division/Department: | Computational and Theoretical Fluid Dynamics Division |
| Depositing User: | Mr. Ravikumar R |
| Date Deposited: | 07 Jul 2006 |
| Last Modified: | 24 May 2010 09:44 |
| URI: | http://nal-ir.nal.res.in/id/eprint/1951 |
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