DA42NG FTD Level 6 Simulator Data Base Part1: Rigid-Body Aerodynamics and Math Model
Jategaonkar, Dr. Ravindra and Fischenberg, Dietrich (2010) DA42NG FTD Level 6 Simulator Data Base Part1: Rigid-Body Aerodynamics and Math Model. DLR-Interner Bericht. DLR-IB 111-2010/25, 226 S.
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The mathematical model pertaining to the rigid-body aircraft motion and the corresponding flight estimated aerodynamic data base for DA42NG are presented in this report. The aerodynamic data base meets the requirements specified by the FAA for a FTD Level 6 simulator in the in-flight regime with both engines operating. The data base includes the three flap configurations, landing gear effects on in-air aerodynamics, and the stall approach regime. The aim of the present report is to provide the simulator manufacturer DSIM adequate details to implement the flight dynamics model. The following aspects are covered in detail: i) Equations of aircraft motion, ii) Rigid-body aerodynamic data base for computing the forces and moments, iii) Flight specific information, iv) Aircraft mass characteristics and v) Demonstration of model fidelity through proof-of-match for FAA specified in-air validation tests.
|Document Type:||Monograph (DLR-Interner Bericht)|
|Title:||DA42NG FTD Level 6 Simulator Data Base Part1: Rigid-Body Aerodynamics and Math Model|
|Number of Pages:||226|
|Keywords:||DA42NG, Rigid-Body Aerodynamics, Math Model|
|HGF - Research field:||no assignement|
|HGF - Program:||Aeronautics|
|HGF - Program Themes:||L AR - Aircraft Research|
|DLR - Research area:||Aeronautics|
|DLR - Program:||L AR - Aircraft Research|
|DLR - Research theme (Project):||L - Systems & Cabin|
|Institutes and Institutions:||Institute of Flight Systems > Flight Dynamics and Simulation|
|Deposited By:||Tanja Bracke|
|Deposited On:||21 Jun 2010 14:21|
|Last Modified:||21 Jun 2010 14:21|
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