26th Congress of International Council of the Aeronautical Sciences
including the 8th AIAA Aviation Technology, Integration, and Operations (ATIO) Conference
14 - 19 September 2008, Anchorage, Alaska, USA
Paper ICAS2008-5.2 ST:

APPLICATION OF A MODEL UPDATING METHOD TO AN AIRCRAFT LONGITUDINAL STABILITY AUGMENTATION SYSTEM

W. S. Mattos, N. C. Pereira, P. C. Greco Jr.
Univ. of São Paulo, Brazil

Keywords: Aircraft Model Updating, Stability Augmentation System, Sensitivity Analysis

The present work describes the application of a model updating method, based on experimental wind tunnel data, to an aircraft longitudinal stability augmentation system. The study includes a revision of model updating methods, the development of aircraft mathematical model and the description of previously conducted aircraft LSAS wind tunnel testing.

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