The identification of aircraft stability and control parameters in turbulence
A technique for the identification of aircraft stability and control parameters from flight test recordings made in either calm or turbulent air is presented. The maximum likelihood output error method is used with a steady-state Kalman filter incorporated to account for atmospheric turbulence. A mo...
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| Language: | en |
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Cranfield University
2016
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| Online Access: | http://dspace.lib.cranfield.ac.uk/handle/1826/10528 |