The identification of aircraft stability and control parameters in turbulence

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dc.contributor.advisor Christopher, P. A. T.
dc.contributor.author Foster, G. W.
dc.date.accessioned 2016-09-14T11:46:02Z
dc.date.available 2016-09-14T11:46:02Z
dc.date.issued 1982-07
dc.identifier.uri http://dspace.lib.cranfield.ac.uk/handle/1826/10528
dc.description.abstract 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 modified Newton-Raphson search technique, enhanced by a line search, is employed for parameter identification. Separate algorithms are developed for estimating the biases and noise levels in the observations. Some areas of practical problems in the application of such methods are stressed. A computer program for the identification of longitudinal stability derivatives is described and the aircraft instrumentation required is exemplified by that in Gnat XPSOS. The wind tunnel calibration of the flow-direction sensing nose probe assembly of Conrad yawmeters on this aircraft is detailed. The problems of handling the flight observations recorded are covered and some of the troubles experienced with the instruments are noted. The performance of the identification technique is investigated. The data required, the choices open to the analyst and the statistical information produced being highlighted. The identification of the process noise level, in this instance the turbulence intensity, is addressed and it is found that the value specified for this level can influence the other parameters. The longitudinal stability and control derivatives obtained for Gnat XPSOS are presented. en_UK
dc.language.iso en en_UK
dc.publisher Cranfield University en_UK
dc.rights © Cranfield University, 1982. All rights reserved. No part of this publication may be reproduced without the written permission of the copyright holder. en_UK
dc.title The identification of aircraft stability and control parameters in turbulence en_UK
dc.type Thesis or dissertation en_UK
dc.type.qualificationlevel Doctoral en_UK
dc.type.qualificationname PhD en_UK


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