Objectives: a) Develop an asymmetric handling qualities metric to predict cross coupling effects of a damaged aircraft: 1) Initial use of U.S Army Aeronautical Design Specification ADS-33; 2) Modification as required based on flight test results. b) Simulation and Flight Validation of proposed metric: 1) F-16 VISTA (March 2010); 2) F-18 Full Scale Test bed (Potential Early Experiment); and 3) Flight Simulators (GTM, ACFS, F-18 HILS). c) Provide flight validated metric and tool box to control law designers.
Flight Validation of a Handling Qualities Metric for a Damaged Aircraft
NASA ARMD/Aviation Safety Technical Conference ; 2009 ; McLean, VA, United States
2009-11-17
Sonstige
Keine Angabe
Englisch
[A Handling Qualities Metric for Damaged Aircraft]
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Large aircraft handling qualities
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