Publication Date:
2019-07-13
Description:
A nonlinear aircraft model is presented and used to develop an overall unified robust and adaptive approach to passive trim and maneuverability envelope estimation with uncertainty quantification. The concept of time scale separation makes this method suitable for the online characterization of altered safe maneuvering limitations after impairment. The results can be used to provide pilot feedback and/or be combined with flight planning, trajectory generation, and guidance algorithms to help maintain safe aircraft operations in both nominal and off-nominal scenarios.
Keywords:
Aircraft Stability and Control; Aircraft Design, Testing and Performance
Type:
ARC-E-DAA-TN11537
,
SciTech 2014; Jan 13, 2014 - Jan 17, 2014; National Harbor, Maryland; United States
Format:
application/pdf
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