The HSCT Flight Controls Group has developed longitudinal control laws, utilizing PTC aeroelastic flexible models to minimize aeroservoelastic interaction effects, for a number of flight conditions. The control law design process resulted in a higher order controller and utilized a large number of sensors distributed along the body for minimizing the flexibility effects. Processes were developed to implement these higher order control laws for performing the dynamic gust loads and flutter analyses. The processes and its validation were documented in Reference 2, for selected flight condition. The analytical results for additional flight conditions are presented in this document for further validation.
Technology Integration (Task 20) Aeroservoelastic Modeling and Design Studies
1999-09-30
Miscellaneous
No indication
English
X-56A MUTT: Aeroservoelastic Modeling
NTIS | 2015
|X-56A MUTT: Aeroservoelastic Modeling
NTRS | 2015
|Examples on increased-order aeroservoelastic modeling
Springer Verlag | 2019
|Robust Aeroservoelastic Design with Structural Variations and Modeling Uncertainties
Online Contents | 2003
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