This paper addresses applied procedures for nonlinear aerodynamic model development and extraction from flight data for the S-3B Viking aircraft. The entire analysis procedures, from dynamic flight test data management to final blending and validation of the upgraded aerodynamic model, was performed within the Integrated Data Evaluation and Analysis Systems (IDEAS) developed by SAIC. IDEAS is a powerful database management system and analysis software containing a full complement of flight data preprocessing, calibration, simulation, model estimation, model verification, and validation tools.
Nonlinear Aerodynamic Model Development and Extraction from Flight Test Data for the S-3B Viking
2000
19 pages
Report
No indication
English
Aerodynamics , Aircraft , Mathematical models , Flight testing , Aerodynamic characteristics , Nonlinear analysis , Antisubmarine aircraft , Data bases , Aerodynamic configurations , Experimental data , Integrated systems , Data management , Validation , Calibration , Computer program verification , Preprocessing , Data base management system , Ideas(Integrated data evaluation and analysis systems) , Ideas data base management system , Flight data , S-3b aircraft , Viking aircraft
AIAA-2001-4015 Nonlinear Aerodynamic Model Extraction from Flight Test Data for the S-3B Viking
British Library Conference Proceedings | 2001
|