Fortran programs for aircraft parameter identification using the estimation-before-modelling technique

dc.contributor.authorHoff, J. C.en_UK
dc.date1997en_UK
dc.date.accessioned2005-11-23T12:21:51Z
dc.date.available2005-11-23T12:21:51Z
dc.date.issued1997en_UK
dc.description.abstractThis report describes five Fortran programs formulated to be used in the Estimation-Before-Modelling (E-B-M) methodology for aircraft parameter estimation. The E-B-M technique is a two step estimation process. In the first step, as formulated in this report, the aircraft states are estimated by using Extended Kalman Filter techniques. In the second step the unknowns aerodynamic derivatives are estimated by linear regression formulated as the Stepwise Regression. The five program comprise two different techniques for state estimation, two algorithms for linear regression and a fixed-lag smoother-differentiator.en_UK
dc.description.sponsorshipThe Universityen_UK
dc.format.extent1963 bytes
dc.format.extent2761448 bytes
dc.format.mimetypetext/plain
dc.format.mimetypeapplication/pdf
dc.identifier.urihttp://hdl.handle.net/1826/213
dc.language.isoen_UKen_UK
dc.relation.ispartofseriesCollege of Aeronautics Report;9709en_UK
dc.relation.ispartofseriesCU/CoA/R;9709en_UK
dc.titleFortran programs for aircraft parameter identification using the estimation-before-modelling techniqueen_UK
dc.typeTechnical Reporten_UK

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