Parameter and performance estimation of an instrumented motor glider was conducted at the National Aeronautics and Space Administration Dryden Flight Research Center in order to provide the necessary information to create a simulation of the aircraft. An output-error technique was employed to generate estimates from doublet maneuvers, and performance estimates were compared with results from a well-known flight-test evaluation of the aircraft in order to provide a complete set of data. Aircraft specifications are given along with information concerning instrumentation, flight-test maneuvers flown, and the output-error technique. Discussion of Cramer-Rao bounds based on both white noise and colored noise assumptions is given. Results include aerodynamic parameter and performance estimates for a range of angles of attack.
AMT-200S Motor Glider Parameter and Performance Estimation
2011
55 pages
Report
Keine Angabe
Englisch
Aircraft , Test Facilities & Equipment , Flight tests , Gliders , Aircraft stability , Aerodynamics , Aircraft control , Aircraft performance , Aircraft maneuvers , Cramer-rao bounds , Angle of attack , Sideslip , Structural weight , Sensors , Backwash , Dynamic response , Equations of motion , Lift drag ratio
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