Stalls and Splines: Current Trends in Flight Testing and Aerodynamic Model Identification

Author:

de Visser Coen C.1,Pool Daan M.1ORCID

Affiliation:

1. Delft University of Technology, 2600 GB Delft, The Netherlands

Abstract

Aerodynamic model identification remains essential for simulator operations and control system design and operations. In this paper, state-of-the-art methodologies for aerodynamic model identification and validation are presented, together with a number of novel applications of the identified models that were recently investigated and developed at the Faculty of Aerospace Engineering of Delft University of Technology. In particular, this paper focuses on methodologies for identifying models of aerodynamic stall from flight data, as well as multivariate spline-based aerodynamic model identification methods, together with their applications in flight simulation and advanced flight control.

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Aerospace Engineering

Reference79 articles.

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2. Anon. “Stall and Stick Pusher Training,” Advisory Circular 120-109, U.S. Department of Transportation, Federal Aviation Administration, Aug. 2012, https://www.faa.gov/documentlibrary/media/advisory_circular/ac%20120-109.pdf [retrieved 8 June 2023].

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