Steinhauser, R. and Looye, G. and Brieger, O. (2004) Design and Evaluation of a Dynamic Inversion Control Law for X-31A. In: Proc. of ODAS 2004, pp. 25-33. 6th ONERA-DLR Aerospace Symposium, Berlin, June 22-23, 2004.
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The Enhanced Fighter Maneuverability of the thrust-vectored X-31A aircraft has already been proven in the German-American (EFM) program in the early nineties . Recently its characteristics with reduced vertical tail were investigated as one of the key research objectives within the German-American VECTOR program. To fulfill this aim the principle of Nonlinear Dynamic Inversion (NDI) has been applied for the primary control law design. NDI is based on the inversion of model equations, so that control laws are easily adapted to varying aircraft configurations and may be generated automatically with the help of advanced modeling tools. The control laws were implemented in the VECTOR fixed-base flight simulator facility. Six experienced pilots assessed and compared flying qualities (for conven-tional as well as post-stall flight conditions) for full and 50% vertical tail configurations.
|Document Type:||Conference or Workshop Item (Paper)|
|Title:||Design and Evaluation of a Dynamic Inversion Control Law for X-31A|
|Journal or Publication Title:||Proc. of ODAS 2004|
|Page Range:||pp. 25-33|
|Keywords:||object-oriented modeling, nonlinear dynamic inversion, vertical tail reduction.|
|Event Title:||6th ONERA-DLR Aerospace Symposium, Berlin, June 22-23, 2004|
|HGF - Research field:||Aeronautics, Space and Transport (old)|
|HGF - Program:||Aeronautics|
|HGF - Program Themes:||Aircraft Research|
|DLR - Research area:||Aeronautics|
|DLR - Program:||L AR - Aircraft Research|
|DLR - Research theme (Project):||UNSPECIFIED|
|Institutes and Institutions:||Institute of Robotics and Mechatronics > System Dynamics and Control (former Control Design Engineering)|
|Deposited By:||elib DLR-Beauftragter|
|Deposited On:||16 Sep 2005|
|Last Modified:||12 Mar 2010 14:19|
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