Ramamoorthy, P (1989) Extended Kalman Filter Algorithm (EKF). Technical Report. National Aerospace Laboratories, Bangalore, India.
![]() |
PDF
tr_pd_cf_8922_R72549.pdf Restricted to Repository staff only Download (276kB) |
![]() |
Indexer Terms (Generate index codes conversion from application/pdf to indexcodes)
indexcodes.txt Restricted to Repository staff only Download (2kB) |
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: | Monograph (Technical Report) |
---|---|
Uncontrolled Keywords: | Kalman filter;Estimation;Short period dynamics |
Subjects: | AERONAUTICS > Aircraft Stability and Control |
Depositing User: | Mr. Ravikumar R |
Date Deposited: | 07 Jul 2006 |
Last Modified: | 24 May 2010 04:14 |
URI: | http://nal-ir.nal.res.in/id/eprint/1951 |
Actions (login required)
![]() |
View Item |