A technique for estimating aerodynamic parameters in real time from flight data without air flow angle measurements is described and demonstrated. The method is applied to simulated F-16 data, and to flight data from a subscale jet transport aircraft. Modeling results obtained with the new approach using flight data without air flow angle measurements were compared to modeling results computed conventionally using flight data that included air flow angle measurements. Comparisons demonstrated that the new technique can provide accurate aerodynamic modeling results without air flow angle measurements, which are often difficult and expensive to obtain. Implications for efficient flight testing and flight safety are discussed.
Real-Time Aerodynamic Parameter Estimation without Air Flow Angle Measurements
AIAA Atmospheric Flight Mechanics Conference ; 2010 ; Toronto, Canada
2010-08-02
Aufsatz (Konferenz)
Keine Angabe
Englisch
Real-Time Aerodynamic Parameter Estimation Without Air Flow Angle Measurements
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