Objectives: () 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
2009
16 pages
Report
No indication
English
[A Handling Qualities Metric for Damaged Aircraft]
NTRS | 2009
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Large aircraft handling qualities
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