A robust nonlinear output feedback control method for limit...

Aerospace Science and Technology 2017 / 05 Vol. 64

A robust nonlinear output feedback control method for limit cycle oscillation suppression using synthetic jet actuators

Ramos-Pedroza, Natalie, MacKunis, William, Golubev, Vladimir
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Volume:
64
Language:
english
Journal:
Aerospace Science and Technology
DOI:
10.1016/j.ast.2016.12.030
Date:
May, 2017
File:
PDF, 669 KB
english, 2017
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