Print Email Facebook Twitter A Multidimensional Spline Based Global Nonlinear Aerodynamic Model for the Cessna Citation II Title A Multidimensional Spline Based Global Nonlinear Aerodynamic Model for the Cessna Citation II Author De Visser, C.C. Mulder, J.A. Faculty Aerospace Engineering Department Control & Operations Date 2010-08-02 Abstract A new method is proposed for the identification of global nonlinear models of aircraft non-dimensional force and moment coefficients. The method is based on a recent type of multivariate spline, the multivariate simplex spline, which can accurately approximate very large, scattered nonlinear datasets in any number of dimensions. The new identification method is used to identify a global nonlinear aerodynamic model of high dimensionality for the Cessna Citation II laboratory aircraft operated by the Delft University of Technology and the Netherlands National Aerospace Laboratory. The data used in the identification process consisted of millions of measurements and was accumulated during more than 250 flight test maneuvers with the laboratory aircraft. The resulting models for the aerodynamic force and moment coefficients are continuous analytical functions as they consist of sets of piecewise defined, multivariate polynomials. The identified models were validated using a subset of the flight data, with validation results showing a very close match between model and reality. To reference this document use: http://resolver.tudelft.nl/uuid:045f1368-3964-4ac7-9626-fbb47da8f277 DOI https://doi.org/10.2514/6.2010-7950 Publisher American Institute of Aeronautics and Astronautics (AIAA) ISBN 978-1-62410-151-9 Source AIAA Atmospheric Flight Mechanics Conference, Toronto, Canada, 2-5 August 2010; AIAA 2010-7950 Part of collection Institutional Repository Document type conference paper Rights © 2010 The Author(s) Files PDF deVisser.pdf 2.3 MB Close viewer /islandora/object/uuid:045f1368-3964-4ac7-9626-fbb47da8f277/datastream/OBJ/view